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Turbulence

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Broader term:

Fluid dynamics

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Used for:

Flow, Turbulent
Turbulent flow

Filed under: Turbulence

On the supremacy of viscosity in the control of turbulent fluid motion. (Catholic University of America, 1956), by Max M. Munk (page images at HathiTrust)
Time constants and frequency response of coated hot wires used as turbulence-sensing elements ([Washingtonm?], 1957), by David W. Taylor Model Basin. Hydromechanics Laboratory and Avis Borden (page images at HathiTrust)
Turbulent diffusion in liquid jets : part I ; measurement of particle concentration by a light scattering probe (For sale by the Supt. of Docs., U.S. G.P.O., 1974), by Charles H. Tinsley, Victor W. Goldschmidt, and Warren S. Stevenson (page images at HathiTrust; US access only)
Turbulent diffusion in liquid jets : final report (For sale by the Supt. of Docs., U.S. G.P.O., 1974), by Strong C. Chaung and Victor W. Goldschmidt (page images at HathiTrust; US access only)
On the motions of particles in turbulent flows (The Commission :, 1980), by S. L. Lee, F. Durst, Universität Karlsruhe, State University of New York at Stony Brook. Department of Mechanical Engineering, and U.S. Nuclear Regulatory Commission. Division of Reactor Safety Research (page images at HathiTrust)
Measurement of aerosol deposition rates in turbulent flows (The Commission, 1980), by J. A. Gieseke, M. A. Goldenberg, K. W. Lee, and Battelle Memorial Institute. Columbus Laboratories (page images at HathiTrust)
Heat transfer to liquid metals in concentric annuli (Oak Ridge National Laboratory, 1950), by Raymond V. Bailey (page images at HathiTrust)
Space and time correlations in a turbulent fluid. (University of California Press, 1954), by J. Bass and Berkeley University of California (page images at HathiTrust; US access only)
Effect of turbulence on vortex-shedding air-velocity transducers (U.S. Dept. of the Interior, Bureau of Mines, 1985), by A. F. Cohen (page images at HathiTrust)
Effect of turbulence promoters on local mass transfer (U.S. Dept. of the Interior; [for sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1970), by P. H. Bradley, F. B. Leitz, J. L. Greatorex, Incorporated Ionics, and United States. Office of Saline Water (page images at HathiTrust)
Combined forced and free turbulent convection in a vertical tube (Argonne National Laboratory, 1962), by Morris S. Ojalvo, R. J. Grosh, U.S. Atomic Energy Commission, and Argonne National Laboratory (page images at HathiTrust)
Turbulent flow (Princeton University Press, 1961), by Galen Brandt Schubauer and Chan Mou Tchen (page images at HathiTrust)
Elementary mechanics of turbulent fluid motion (Catholic University of America, 1960), by Max Michael Munk (page images at HathiTrust)
Studies of the spectra of the vertical fluxes of momentum, heat, and moisture in the atmospheric boundary layer : annual report (Division of Sponsored Research, M.I.T. Meteorology Dept., Round Hill Field Station, 1961), by H. E. Cramer and Massachusetts Institute of Technology. Round Hill Field Station (page images at HathiTrust)
Power spectrum analyses of turbulent surface winds over water under inversion conditions (New York University, College of Engineering, Research Division, Dept. of Meteorology and Oceanography, 1961), by Joseph Pandolfo and New York University. School of Engineering and Science (page images at HathiTrust)
The development of an observational system for turbulent wind, temperature and humidity measurements over coastal waters (Research Division, College of Engineering, New York University, Dept. of Meteorology and Oceanography, 1962), by Joseph Pandolfo and New York University. School of Engineering and Science (page images at HathiTrust)
Oceanic turbulence (review) (Oceanographic Institute, Florida State University, 1962), by Takashi Ichiye (page images at HathiTrust)
The role of clouds and oceans in global greenhouse warming : progress report to the Department of Energy (s.n.], 1991), by Martin I Hoffert (page images at HathiTrust)
Surface pressure fluctuations near an axisymmetric stagnation point (U.S. National Bureau of Standards :, 1971), by Richard D. Marshall (page images at HathiTrust)
Turbulence modeling and sediment transport (U.S. Army Engineer Waterways Experiment Station, 1997), by Fabian Lopez, Marcelo Garcia, Wetlands Research Program (U.S.), U.S. Army Engineer Waterways Experiment Station, and United States Army Corps of Engineers (page images at HathiTrust)
Effect of wire wraps on pressure drop for axial turbulent flow through rod bundels (U.S. Atomic Energy Commission, 1963), by E. D. Waters, United States. National Bureau of Standards, United States. Department of Energy. Office of Fusion Energy, United States. National Bureau of Standards. Fracture and Deformation Division, U.S. Atomic Energy Commission, United States. Energy Research and Development Administration, Hanford Works, and Hanford Atomic Products Operation (page images at HathiTrust)
The regeneration of surface waves by wind in interactions with internal gravity waves (Hydronautics, Inc., 1973), by O. M. Phillips and inc Hydronautics (page images at HathiTrust)
The statistical theory of turbulence : seminar on fluid mechanics, Department of Civil Engineering (Northwestern University, Technological Institute, 1957), by William H. Reid and Ill.). Technological Institute. Dept. of Civil Engineering Northwestern University (Evanston (page images at HathiTrust)
A numerical solution for the interaction of a moving shock wave with a turbulent mixing region (Issued by Sandia Corp.], 1966), by William Fred Walker and Glen W. Zumwalt (page images at HathiTrust; US access only)
Plasma turbulence. (Physical Research Laboratory, Space Technology Laboratories, Inc., 1960), by Leslie S. G. Kovásznay (page images at HathiTrust)
Formulation of the theory of turbulence in an incompressible fluid. (Physics Dept., University of Illinois;, 1961), by H. W. Wyld (page images at HathiTrust)
Hot-wire measurements with X-meters (Graduate School of Aeronautical Engineering, Cornell University, 1955), by Harry Israel Ashkenas (page images at HathiTrust)
A technical report on turbulent mixing in a partially ionized gas. (Princeton, N.J., 1962), by Princeton University. Guggenheim Laboratories for the Aerospace Propulsion Sciences and Paul F. Jacobs (page images at HathiTrust)
Technical report on the spectrum of turbulence in an exothermal gas flow (GM Defense Research Laboratories, Aerospace Operations Dept., 1963), by Alan Eschenroeder, Tong Chen, and Santa Barbara General Motors Corporation. Defense Research Laboratories (page images at HathiTrust)
Technical report on intensification of turbulence by chemical heat release. Contract no. DA-04-495-ORD-3567(Z) Hypervelocity Range Research Program, a part of project "Defender." (GM Defense Research Laboratories, Aerospace Operations Dept., 1963), by Alan Eschenroeder and Santa Barbara General Motors Corporation. Defense Research Laboratories (page images at HathiTrust)
Thermal agitation and turbulence. (Physical Research Laboratory, Space Technology Laboratories, 1960), by R. Betchov (page images at HathiTrust)
Symposium on turbulence, 1 July, 1949; a joint meeting with the Fluid Dynamics Division of the American Physical Society. (Silver Spring, Md., 1950), by Md.) Naval Ordnance Laboratory (White Oak and American Physical Society. Division of Fluid Dynamics (page images at HathiTrust; US access only)
The theories of turbulence (NACA, 1955), by L. Agostini, J. Bass, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Comparison of turbulent wake characteristics with different eddy viscosity coefficients (Missile and Space Division, General Electric, 1963), by K. S. Wan and Philadelphia General Electric Company. Space Sciences Laboratory (page images at HathiTrust)
Some data on diffusion and turbulence in relation to reaeration : final report (University of Illinois, Water Resources Center, 1969), by Edward R. Holley and University of Illinois at Urbana-Champaign. Water Resources Center (page images at HathiTrust)
Calculation of reattaching shear layers in divergent channel with a multiple-time-scale turbulence model (National Aeronautics and Space Administration ;, 1989), by S. -W. Kim and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)
Multiscale turbulence effects in supersonic jets exhausting into still air (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Khaled S. Abdol-Hamid, Richard G. Wilmoth, and Langley Research Center (page images at HathiTrust)
Effect of Reynolds number variation on aerodynamics of a hydrogen-fueled transport concept at Mach 6 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by Jim A. Penland, Don C. Marcum, and Langley Research Center (page images at HathiTrust)
Application of turbulence modeling to predict surface heat transfer in stagnation flow region of circular cylinder (National Aeronautics and Space Administration, 1987), by Chi R. Wang, Frederick C. Yeh, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Remarks on turbulent constitutive relations (Institute for Computational Mechnics in Propulsion and Center for Modeling of Turbulence and Transition, Lewis Research Center ;, 1993), by Tsan-Hsing Shih, John L. Lumley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Broken symmetry in ideal magnetohydrodynamic turbulence (National Aeronautics and Space Administration, Langley Research Center ;, 1993), by John V. Shebalin and Langley Research Center (page images at HathiTrust)
NASA supercritical airfoils : a matrix of family-related airfoils (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Charles D. Harris and Langley Research Center (page images at HathiTrust)
Calculations of turbulent separated flows (National Aeronautics and Space Administration ;, 1993), by J. Zhu, T. H. Shih, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A vorticity dynamics based model for the turbulent dissipation : model development and validation (National Aeronautics and Space Administration ;, 1994), by Tsan-Hsing Shih and United States National Aeronautics and Space Administration (page images at HathiTrust)
A realizable Reynolds stress algebraic equation model (National Aeronautics and Space Administration, 1993), by Tsan-Hsing Shih, John L. Lumley, Jiang Zhu, Lewis Research Center, and Japan) Symposium on Turbulence Shear Flows : (Ninth : 1993 : Kyoto (page images at HathiTrust)
Comparison of PDF and moment closure methods in the modeling of turbulent reacting flows (National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion ;, 1994), by Andrew T. Norris, Andrew T. Hsu, and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)
Turbulent magnetohydrodynamic flows in prismatic and cylindrical pipes (], 1967), by Herman Branover, A. B. T︠S︡inober, and I︠U︡. M. Gelʹfgat (page images at HathiTrust)
A new k-[epsilon] eddy viscosity model for high Reynolds number turbulent flows : model development and validation (National Aeronautics and Space Administration ;, 1994), by United States National Aeronautics and Space Administration (page images at HathiTrust)
Kolmogorov behavior of near-wall turbulence and its application in turbulence modeling (National Aeronautics and Space Administration ;, 1992), by Tsan-Hsing Shih, John L. Lumley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A k-E [i.e. Kappa-Epsilon] calculation of transitional boundary layers (NASA ;, 1992), by Z. Yang, T. H. Shih, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Elliptic flow computation by low Reynolds number two-equation turbulence models (National Aeronautics and Space Administration ;, 1991), by V. Michelassi, T.-H. Shih, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by Jacob H. Lichtenstein, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Considerations for the installation of honeycomb and screeens to reduce wind-tunnel turbulence (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by James Scheiman, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
Three-dimensional turbulent-mixing-length modeling for discrete-hole coolant injection into a crossflow (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Chi R. Wang, S. Stephen Papell, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Effect of collector configuration on test section turbulence levels in an open-jet wind tunnel (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by G. S. Manuel, P. S. Barna, John K. Molloy, and Langley Research Center (page images at HathiTrust)
Application of a two-dimensial parabolic computer program to prediction of turbulent reacting flows (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by John S. Evans, H. L. Beach, Charles J. Schexnayder, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Design and experimental results for a flapped natural-laminar-flow airfoil for general aviation applications (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Dan M. Somers and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Background noise measurements from jet exit vanes designed to reduce flow pulsations in an open-jet wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Danny R. Hoad, R. M. Martin, United States. Army Aviation Systems Command. Structures Laboratory, and Langley Research Center (page images at HathiTrust)
Implicit solution of three-dimensional internal turbulent flows (National Aeronautics and Space Administration ;, 1990), by V. Michelassi, M.-S. Liou, Louis A. Povinelli, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Comparison of experimental and theoretical turbulance reduction characteristics for screens, honeycomb, and honeycomb-screen combinations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by James Scheiman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model (National Aeronautics and Space Administration ;, 1990), by S. W. Kim, Lewis Research Center. Institute for Computational Mechanics in Propulsion, and United States National Aeronautics and Space Administration (page images at HathiTrust)
An improved [k-epsilon] model for near-wall turbulence and comparison with direct numerical simulation (National Aeronautics and Space Administration ;, 1990), by T. H. Shih and United States National Aeronautics and Space Administration (page images at HathiTrust)
Low Reynolds number two equation modeling of turbulent flows (NASA ;, 1991), by V. Michelassi, T.-H. Shih, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Second order modeling of boundary-free turbulent shear flows (NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion ;, 1991), by T. H. Shih, J. L. Limley, J. Y. Chen, and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)
Advances in modeling the pressure correlation terms in the second moment equations (National Aeronautics and Space Administration ;, 1991), by Tsan-Hsing Shih, John L. Lumley, Aamir Shabbir, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Numerical solutions of the Navier-Stokes equations for transonic afterbody flows (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1980), by R. Charles Swanson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
A near-wall turbulence model and its application to fully developed turbulent channel and pipe flows (National Aeronautics and Space Administration ;, 1988), by S. W. Kim and United States National Aeronautics and Space Administration (page images at HathiTrust)
Wall-layer eruptions in turbulent flows (National Aeronautics and Space Administration ;, 1989), by J. D. A. Walker and United States National Aeronautics and Space Administration (page images at HathiTrust)
Center for Modeling of Turbulence and Transition (CMOTT) : research briefs, 1990. (National Aeronautics and Space Administration, 1991), by United States National Aeronautics and Space Administration (page images at HathiTrust)
Phase development and its role on subharmonic control (National Aeronautics and Space Administration ;, 1989), by Reda R. Mankbadi, Edward J. Rice, Ganesh Raman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Design and experimental results for a Natural-Laminar-Flow airfoil for general aviation application (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Dan M. Somers, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Subsonic sphere drag measurements at intermediate Reynolds numbers (National Aeronautics and Space Administration ;, 1969), by Kenneth R. Sivier, J. A. Nicholls, University of Michigan. Dept. of Aerospace Engineering, and Lewis Research Center (page images at HathiTrust)
Review of current status of prediction techniques (National Aeronautics and Space Administration ;, 1972), by Richard E. Hayden, Langley Research Center, and Beranek Bolt (page images at HathiTrust)
Theoretical study of vortex shedding from bodies of revolution undergoing coning motion (National Aeronautics and Space Administration ;, 1969), by Gary D. Kuhn, Jack N. Nielsen, Selden B. Spangler, Ames Research Center, and Inc Nielsen Engineering & Research (page images at HathiTrust)
Sonic boom in turbulence (National Aeronautics and Space Administration ;, 1971), by W. A. Horning, United States National Aeronautics and Space Administration, Langley Research Center, and inc EG & G (page images at HathiTrust)
Numerical investigation of an internal layer in turbulent flow over a curved hill (NASA Lewis Research Center ;, 1989), by S. W. Kim and Lewis Research Center (page images at HathiTrust)
Experimental determination of pressure drop and flow characteristics of dilute gas-solid suspensions (National Aeronautics and Space Administration ;, 1971), by Robert Pfeffer, Salvatore J. Rossetti, Lewis Research Center, and City University of New York. City College (page images at HathiTrust)
Fluid entrainment (National Aeronautics and Space Administration, 1964), by Jacques A. F. Hill, James E. Nicholson, Inc Mithras, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Calculation of two-dimensional turbulent flow fields (National Aeronautics and Space Administration, 1966), by John G. Trulio (page images at HathiTrust; US access only)
Investigation of the turbulent shear flow of dilute aqueous CMC solutions (National Aeronautics and Space Administration, 1966), by W. D. Ernst (page images at HathiTrust; US access only)
Analytical investigation of incompressible turbulent swirling flow in pipes (The Institute, 1968), by Avelino Parcon Rochino, Z. Lavan, Lewis Research Center, and Illinois Institute of Technology (page images at HathiTrust; US access only)
Wave theory of turbulence in compressible media (U.S. National Aeronautics and Space Administration ;, 1976), by Czeslaw P. Kentzer, United States National Aeronautics and Space Administration, Langley Research Center, and Purdue University (page images at HathiTrust)
A wind model for an elevated stol-port configuration (National Aeronautics and Space Administration, 1974), by J. A. Peterka, J. E. Cermak, Ames Research Center, and Colorado State University (page images at HathiTrust)
Acoustic radiation and surface pressure characteristics of an airfoil due to incident turbulence (National Aeronautics and Space Administration ;, 1976), by Robert W. Paterson, Roy K. Amiet, United Technologies Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Discrete wall jets in quiescent air (National Aeronautics and Space Administration ;, 1974), by J. D. McLean, H. J. Herring, Lewis Research Center, and Princeton University (page images at HathiTrust)
Experiments on confined turbulent jets in cross flow (National Aeronautics and Space Administration ;, 1974), by Yasuhiro Kamotani, Isaac Greber, Lewis Research Center, and Case Western Reserve University (page images at HathiTrust)
Finite-difference solution for turbulent swirling compressible flow in axisymmetric ducts with struts (National Aeronautics and Space Administration ;, 1974), by O. L. Anderson, Lewis Research Center, and United Aircraft Corporation (page images at HathiTrust)
Turbulent mixing in the initial region of heterogeneous axisymmetric coaxial confined jets (National Aeronautics and Space Administration, 1970), by Kirti N. Ghia, Zalman Lavan, T. Paul Torada, United States National Aeronautics and Space Administration, Lewis Research Center, and Illinois Institute of Technology (page images at HathiTrust)
Theoretical frequency response functions and power spectra of the XB-70 response to atmospheric turbulence (National Aeronautics and Space Administration, 1970), by Thomas E. Stenton, United States National Aeronautics and Space Administration, Langley Research Center, and North American Rockwell Corporation (page images at HathiTrust)
Observation of flow excursions in a simulated gas-cooled reactor passage (National Aeronautics and Space Administration ;, 1970), by Paul Vingerhoet, Eli Reshotko, Edward R. Kolbe, Lewis Research Center, and Case Western Reserve University (page images at HathiTrust)
NASA CR-1523 (National Aeronautics and Space Administration ;, 1970), by Richard F. Porter, Joe H. Brown, United States National Aeronautics and Space Administration, Ames Research Center, and Battelle Memorial Institute (page images at HathiTrust)
Dynamic response of high-frequency pressure transducers to large amplitude sinusoidal pressure oscillations (National Aeronautics and Space Administration ;, 1972), by Richard E. Robinson, Lewis Research Center, and Battelle Memorial Institute (page images at HathiTrust)
Recirculation patterns in the initial region of coaxial jets (National Aeronautics and Space Administration ;, 1970), by Tzvi Rozenman, Herbert Weinstein, Lewis Research Center, and Illinois Institute of Technology. Dept. of Chemical Engineering (page images at HathiTrust)
A symmetrical laser Doppler velocity meter and its application to turbulence characterization (National Aeronautics and Space Administration, 1972), by Malay Kumar Mazumder, Ames Research Center, and Fayetteville. Graduate Institute of Technology University of Arkansas (page images at HathiTrust)
Experimental investigation of model variable-geometry and ogee tip rotors (National Aeronautics and Space Administration ;, 1974), by Anton J. Landgrebe, E. Dean Bellinger, Langley Research Center, and United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
Multiple-scale turbulence modeling of boundary layer flows for scramjet applications (National Aeronautics and Space Administration, Scientific and Technical Information Branch;, 1981), by G. Fabris, R. B. Edelman, P. T. Harsha, inc. Combustion Science and Advanced Technology Dept Science Applications, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
A review of the theory of trailing edge noise (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), by M. S. Howe, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Development of a three-dimensional turbulent duct flow analysis (National Aeronautics and Space Administration, Scientific and Technical Information Office. ;, 1978), by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, P. R. Eiseman, Lewis Research Center, and United Technologies Research Center (page images at HathiTrust)
Experimental study of superlaminar flow between nonconcentric rotating cylinders (National Aeronautics and Space Administration, 1967), by John Vohr (page images at HathiTrust; US access only)
Three-dimensional compressible turbulent computations for a diffusing S-duct (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by C. F. Smith, Lewis Research Center, and Inc Sverdrup Technology (page images at HathiTrust)
Research on instabilities in atmospheric flow systems associated with clear air turbulence (National Aeronautics and Space Administration, 1970), by James W. Clark, Paul G. Vogt, Richard C. Stoeffler, United States National Aeronautics and Space Administration, and United Aircraft Corporation (page images at HathiTrust)
Three-dimensional compressible turbulent computations for a nondiffusing S-duct (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by G. J. Harloff, Lewis Research Center, and Inc Sverdrup Technology (page images at HathiTrust)
Assessment of turbulence models for scramjet flowfields (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by M. M. Sindir, P. T. Harsha, inc. Combustion Science and Advanced Technology Dept Science Applications, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Investigation of the vibration isolation of commercial jet transport pilots during turbulent air penetration (National Aeronautics and Space Administration, 1970), by Dale W. Schubert, Frank E. Roman, Jerome S. Pepi, United States National Aeronautics and Space Administration, Langley Research Center, and Barry Wright Corporation (page images at HathiTrust)
Premixing quality and flame stability : a theoretical and experimental study (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Krishnan Radhakrishnan, Rodney J. Tabacynski, John B. Heywood, Massachusetts Institute of Technology, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
An experimental study of near wall flow parameters in the blade end-wall corner region (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1989), by Rakesh K. Bhargava, Rishi S. Raj, and Lewis Research Center (page images at HathiTrust)
Effects of mach number and wall-temperature ratio on turbulent heat transfer at mach numbers from 3 to 5 (U.S. G.P.O.], 1959), by Thorval Tendeland (page images at HathiTrust)
Calculations of compressible average turbulent skin friction (National Aeronautics and Space Administration ;, 1962), by Mitchel H. Bertram (page images at HathiTrust)
NASA TR R-267 (National Aeronautics and Space Administration ;, 1967), by Maynard F. Taylor, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Heat transfer and pressure drop in blade cooling channels with turbulence promoters (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by J. C. Han, C. K. Lei, J. S. Park, Lewis Research Center, and Texas A & M University. Dept. of Mechanical Engineering (page images at HathiTrust)
Analysis of the injection of a heated turbulent jet into a cross flow (National Aeronautics and Space Administration, 1973), by James F. Campbell, Joseph A. Schetz, and Langley Research Center (page images at HathiTrust)
Analysis of multipoint-multitime correlations and diffusion in decaying homogeneous turbulence (U.S. G.P.O.], 1961), by Robert G. Deissler (page images at HathiTrust)
Induced pressure distribution of a jet in a crossflow (National Aeronautics and Space Administration ;, 1975), by Richard L. Fearn, Robert P. Weston, and Langley Research Center (page images at HathiTrust)
Effect of free-stream turbulence on film cooling (National Aeronautics and Space Administration ;, 1975), by Cecil J. Marek, Robert R. Tacina, and Lewis Research Center (page images at HathiTrust)
Evolution of amplified waves leading to transition in a boundary layer with zero pressure gradient (National Aeronautics and Space Administration, 1959), by P. S. Klebanoff, K. D. Tidstrom, and United States. National Bureau of Standards (page images at HathiTrust)
NASA TN D-2511 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), by Jay Fox, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-2501 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), by Jay Fox, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Effect of uniform longitudinal strain rate on weak homogeneous turbulence in a compressible flow (National Aeronautics and Space Administration, 1965), by Robert G. Deissler and United States National Aeronautics and Space Administration (page images at HathiTrust)
Experimental study of a free turbulent shear flow at Mach 19 with electron-beam and conventional probes (National Aeronautics and Space Administration ;, 1975), by William D. Harvey, William W. Hunter, and Langley Research Center (page images at HathiTrust)
Atmospheric turbulence measurements obtained from airplane operations at altitudes between 20,000 and 75,000 feet for several areas in the Northern Hemisphere (National Aeronautics and Space Administration, 1960), by Thomas L. Coleman, Roy Steiner, and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-5753 (National Aeronautics and Space Administration ;, 1969), by Charles B. Johnson, Dennis M. Bushnell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Distribution of time-averaged pressure fluctuations along the boundary of a round subsonic jet (National Aeronautics and Space Administration :, 1960), by Walton L. Howes and Lewis Research Center (page images at HathiTrust)
Aerodynamic characteristics of vehicle bodies at crosswind conditions in ground proximity (National Aeronautics and Space Administration, 1970), by Kalman J. Grunwald, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Evaluation of the effect of a yaw-rate damper on the flying qualities of a light twin-engine airplane (National Aeronautics and Space Administration :, 1970), by Calvin R. Jarvis, Einar K. Enevoldson, Paul C. Loschke, United States National Aeronautics and Space Administration, and Flight Research Center (U.S.) (page images at HathiTrust)
An experimental investigation of the velocity fluctuations behind oscillating vanes (National Aeronautics and Space Administration ;, 1970), by Donald A. Buell, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
Application of various techniques for determining local heat-transfer coefficients in a rocket engine from transient experimental data (National Aeronautics and Space Administration, 1960), by Curt H. Liebert, Ronald W. Grant, James E. Hatch, and Lewis Research Center (page images at HathiTrust)
Flight measurement of wall-pressure fluctuations and boundary-layer turbulence (National Aeronautics and Space Administration, 1960), by Harold R. Mull, Joseph S. Algranti, and Lewis Research Center (page images at HathiTrust)
Investigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds (National Aeronautics and Space Administration, 1960), by Mary W. Jackson, K. R. Czarnecki, and Langley Research Center (page images at HathiTrust)
NASA TN D-5826 (National Aeronautics and Space Administration :, 1970), by Richard A. Martin, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
NASA TN D-6728 (National Aeronautics and Space Administration :, 1972), by Robert G. Deissler, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Turbulence, heat-transfer, and boundary layer measurements in a conical nozzle with a controlled inlet velocity profile (National Aeronautics and Space Administration :, 1966), by Donald R. Boldman, Anthony Fortini, James F. Schmidt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Measurements of pressure and local heat transfer on a 20 degree cone at angles of attack up to 20 degrees for a mach number of 4.95 (National Aeronautics and Space Administration :, 1959), by Jerome D. Julius and United States National Aeronautics and Space Administration (page images at HathiTrust)
NASA TN D-3779 (National Aeronautics and Space Administration :, 1967), by Robert G. Deissler and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Shock-tube heat-transfer measurements on inner surface of a cylinder (simulating a flat plate) for stagnation-temperature range 4,100 ̊to 8,300 ̊R (National Aeronautics and Space Administration, 1959), by Jim J. Jones and Langley Research Center (page images at HathiTrust)
Investigation of effects of roughness, surface cooling, and shock impingement on boundary-layer transition on a two-dimensional wing (National Aeronautics and Space Administration :, 1960), by K. R. Czarnecki, John R. Sevier, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Mixing of wakes in a turbulent shear flow (National Aeronautics and Space Administration, 1959), by Salamon Eskinazi and Syracuse University (page images at HathiTrust)
Vibration and near-field sound of thin-walled cylinders caused by internal turbulent flow (National Aeronautics and Space Administration, 1960), by Paul F. R. Weyers and California Institute of Technology (page images at HathiTrust)
Local turbulent heat transfer for water in entrance regions of tubes with various unheated starting lengths (National Aeronautics and Space Administration ;, 1965), by James R. Stone and Lewis Research Center (page images at HathiTrust)
An experimental investigation of a highly underexpanded sonic jet ejecting from a flat plate into a subsonic crossflow (National Aeronautics and Space Administration ;, 1973), by Craig S. Shaw, Richard J. Margason, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Analysis of internal flow characteristics of a smooth-disk water-brake dynamometer (National Aeronautics and Space Administration ;, 1973), by David G. Evans and Lewis Research Center (page images at HathiTrust)
Retrieval of dispersive and convective transport phenomena in fluids using stationary and nonstationary time domain analysis (National Aeronautics and Space Administration ;, 1973), by J. Briscoe Stephens, Robert M. St. John, United States National Aeronautics and Space Administration, and George C. Marshall Space Flight Center (page images at HathiTrust)
Study of the wind profile in the lowest 400 feet of the atmosphere : progress report no. ... (Brookhaven National Laboratory, 1958), by Irving A. Singer, Gilbert S. Raynor, Brookhaven National Laboratory, U.S. Atomic Energy Commission, and U.S. Army Signal Research and Development Laboratory (page images at HathiTrust)
Turbulent liquid-metal heat transfer in concentric annuli with axially varying heat flux (Brookhaven National Laboratory, 1969), by W. S. Yu, John C. Chen, Brookhaven National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
Location of separation on a circular cylinder in crossflow as a function of Reynolds Number (Naval Ship Research and Development Center, 1971), by David W. Coder and Naval Ship Research and Development Center (page images at HathiTrust)
Report on investigation of developed turbulence (National Advisory Commitee for Aeronautics ;, 1949), by Ludwig Prandtl and United States. National Advisory Commitee for Aeronautics (page images at HathiTrust)
The microstructure of turbulent flow (NACA, 1953), by A. M. Obukhoff, A. M. I�Aglom, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
On stability and turbulence of fluid flows (NACA, 1951), by Werner Heisenberg and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Lecture series "boundary layer theory." Part II, turbulent flows (NACA, 1949), by H. Schlichting and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Preliminary report on a study of separated flows in supersonic and subsonic streams (National Advisory Committee for Aeronautics, 1956), by Dean R. Chapman, Howard K. Larson, Donald M. Kuehn, United States National Advisory Committee for Aeronautics, and Ames Research Center (page images at HathiTrust)
On the statistical theory of turbulence (National Advisory Committee for Aeronautics, 1958), by Werner Heisenberg and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Mixing-length formulations for turbulent boundary layers over arbitrarily rough surfaces (David W. Taylor Naval Ship Research and Development Center, 1984), by Paul S. Granville and David W. Taylor Naval Ship Research and Development Center (page images at HathiTrust)
Is there a Helmholtz mixing coefficient? (Los Alamos Scientific Laboratory of the University of California, 1953), by R. L. Ingraham, John Archibald Wheeler, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
Some considerations on Helmholtz instability (Los Alamos Scientific Laboratory of the University of California, 1953), by E. A. Frieman, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
Operations Division. (Oak Ridge National Laboratory, 1949), by E. M. Sparrow, Oak Ridge National Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
1973-1977 rough rider turbulence-radar intensity study : final report (Federal Aviation Administration, Systems Research and Development Service ;, 1979), by J. T. Lee, D. Carpenter, National Severe Storms Laboratory, and United States. Federal Aviation Administration. Systems Research and Development Service (page images at HathiTrust)
Rules of thumb for avoiding or minimizing encounters with clear air turbulence. (Federal Aviation Administration, 1988), by United States Federal Aviation Administration (page images at HathiTrust)
Center for Modeling of Turbulence and Transition (CMOTT) : research briefs, 1992 (National Aeronautics and Space Administration, 1992), by United States National Aeronautics and Space Administration (page images at HathiTrust)
Effect of turbulence on vortex-shedding air-velocity transducers (U.S. Dept. of the Interior, Bureau of Mines, 1985), by A. F. Cohen (page images at HathiTrust)
Mixing in turbulent flow (University of Illinois, 1951), by University of Illinois (Urbana-Champaign campus). Engineering Experiment Station, Henry Fraser Johnstone, and Arnold Kivnick (page images at HathiTrust)
Growth of disturbances in a flame-generated shear region (National Advisory Committee for Aeronautics, 1956), by Perry L. Blackshear and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Influence of external variables on smoking of benzene flames (National Advisory Committee for Aeronautics, 1952), by Thomas P. Clark, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
Correlation of turbulent heat transfer in a tube for the dissociating system N204 <==> 2N02. (National Advisory Committee for Aeronautics, 1958), by Richard S. Brokaw, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Airplane motions and loads induced by flying through the flow field generated by an airplane at low supersonic speeds (National Advisory Committee for Aeronautics, 1957), by Gareth H. Jordan, Stanley P. Butchart, Earl R. Keener, Flight Research Center (U.S.), United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Investigation of a simple device for preventing separation due to shock and boundary-layer interaction (National Advisory Committee for Aeronautics, 1950), by Coleman duP. Donaldson, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Factors affecting transition at supersonic speeds (National Advisory Committee for Aeronautics, 1953), by K. R. Czarnecki, Archibald R. Sinclair, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Investigation with an interferometer of the turbulent mixing of a free supersonic jet (National Advisory Committee for Aeronautics, 1949), by Paul B. Gooderum, Maurice J. Brevoort, George P. Wood, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
An evaluation of the use of ground radar for avoiding severe turbulence associated with thunderstorms (National Advisory Committee for Aeronautics, 1949), by J. K. Thompson, V. W. Lipscomb, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Investigation of turbulent flow in a two-dimensional channel (National Advisory Committee for Aeronautics, 1950), by John Laufer and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Investigation of separation of the turbulent boundary layer (National Advisory Committee for Aeronautics, 1950), by G. B. Schubauer, P. S. Klebanoff, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Analytical investigation of turbulent flow in smooth tubes with heat transfer with variable fluid properties for Prandtl number of 1 (National Advisory Committee for Aeronautics, 1950), by Robert G. Deissler and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Spectrum of turbulence in a contracting stream (National Advisory Committee for Aeronautics, 1952), by Herbert Spencer Ribner, Maurice Tucker, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Diffusion of heat from a line source in isotropic turbulence (National Advisory Committee for Aeronautics, 1952), by M. S. Uberoi, Stanley Corrsin, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Average skin-friction drag coefficients from tank tests of a parabolic body of revolution (NACA RM-10) (National Advisory Committee for Aeronautics, 1953), by Elmo J. Mottard, J. Dan Loposer, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Correlation of calculation and flight studies of the effect of wing flexibility on structural response due to gusts (National Advisory Committee for Aeronautics, 1953), by John C. Houbolt and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Analysis of turbulent heat transfer, mass transfer, and friction in smooth tubes at high Prandtl and Schmidt numbers (National Advisory Committee for Aeronautics, 1954), by Robert G. Deissler and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Radial variation of eddy diffusivity tensor components for three-dimensional mass transport (Ames Laboratory, Iowa State University of Science and Technology, 1964), by Alvin Eugene Konopik, Ray Fahien, Ames Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
Simultaneous single element air temperature and velocity measurements (United States Atomic Energy Commission, Technical Information Service, 1957), by James E. Benjamin, Ray W. Fahien, Ames Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
Analysis of turbulent heat transfer and flow in the entrance regions of smooth passages (National Advisory Committee for Aeronautics, 1953), by Robert G. Diessler, Lewis Research Center, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Analytical solution for the wind-driven circulation in a lake containing an island / by Marvin E. Goldstein and Richard T. Gedney. (National Aeronautics and Space Administration, 1971), by Marvin E. Goldstein, Richard T. Gedney, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Characteristics of loads in rough air at transonic speeds of rocket-powered models of a canard and a conventional-tail configuration (National Advisory Committee for Aeronautics, 1955), by A. James Vitale and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Study of the pressure rise across shock waves required to separate laminar and turbulent boundary layers (National Advisory Committee for Aeronautics, 1952), by Coleman duP. Donaldson, Roy H. Lange, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
APEX-391 (General Electric, Atomic Products Division, Aircraft Nuclear Propulsion Dept., 1958), by J. F. Heyda and General Electric Company. Aircraft Nuclear Propulsion Department (page images at HathiTrust)
Turbulent mixing of axisymmetric compressible jets : (in the half-jet region) with quiescent air (Sandia Corp. ;, 1963), by R. C. Maydew, J. F. Reed, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust; US access only)
Contribution to the calculation of turbulent boundary layers. (Navy Dept., David W. Taylor model basin], 1951), by Julius C. Rotta (page images at HathiTrust)
Two-equation, depth-integrated turbulence closure for modeling geometry-dominated flows (U.S. Army Engineer Waterways Experiment Station, 1983), by Raymond S. Chapman, Environmental Laboratory (U.S. Army Engineer Waterways Experiment Station), and United States Army Corps of Engineers (page images at HathiTrust)
Tests in the Variable Density Wind Tunnel to investigate the effects of scale and turbulence on airfoil characteristics (National Advisory Committee for Aeronautics ;, 1931), by John Stack and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Preliminary study of applied load factors in bumpy air (National Advisory Committee for Aeronautics ;, 1931), by Richard V. Rhode, Eugene E. Lundquist, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Velocity profiles and friction factors for turbulent pipe flow with uniform wall suction (Union Carbide Nuclear Company, 1956), by H. L. Weissberg, Union Carbide Nuclear Company, U.S. Atomic Energy Commission, and Oak Ridge Gaseous Diffusion Plant (page images at HathiTrust)
Pressure loss and heat transfer for turbulent flow. (U. S. Atomic Energy Commission, Office of Technical Information, 1960), by Rudolph Koch (page images at HathiTrust)
Interaction of waves and currents (Fort Belvoir, Virginia : U.S. Army, Corps of Engineers, Coastal Engineering Research Center, 1983., 1983), by D. H. Peregrine, Cyril J. Galvin, Ivar G. Jonsson, and Coastal Engineering Research Center (U.S.) (page images at HathiTrust)
Sediment suspension and turbulence in an oscillating flume (Fort Belvoir, Virginia : U.S. Army Coastal Engineering Research Center ; Springfield, Virginia : National Technical Information Service, Operations Division, 1977., 1977), by Thomas C. MacDonald, Berkeley. Hydraulic Engineering Laboratory University of California, and Coastal Engineering Research Center (U.S.) (page images at HathiTrust)
On the measurement of pressure fluctuations at the smooth boundary of an incompressible turbulent flow (University of California, Institute of Engineering Research, 1954), by Huon Li and Berkeley. Institute of Engineering Research University of California (page images at HathiTrust; US access only)
Turbulence investigations in liquid shear flow by the method of electromagnetic induction (University of California, Institute of Engineering Research, 1956), by Lawrence Morton Grossman, Huon Li, and Berkeley. Institute of Engineering Research University of California (page images at HathiTrust; US access only)
On the measurement of turbulent pressure fluctuations with a transducer of finite size (University of California, Institute of Engineering Research, 1959), by Gillis M. Corcos, W. A. Von Winkle, J. W. Cuthbert, and Berkeley. Institute of Engineering Research University of California (page images at HathiTrust; US access only)
Viscous dissipation in turbulent motion (The Catholic University of America, 1956), by Max M. Munk (page images at HathiTrust; US access only)
Turbulence theory in the light of the circular pipe flow (U.S. Dept. of Aeronautical and Mechanical Engineering, distributor, 1957), by Max M. Munk (page images at HathiTrust; US access only)
Hydraulic characteristics of gate slots (Bureau of Reclamation, 1958), by J. W. Ball (page images at HathiTrust; US access only)
Turbulent flow in eccentric annuli (San Jose, California : General Electric Company, Atomic Power Equipment Department, 1966., 1966), by Alan Eugene Rogers, U.S. Atomic Energy Commission, and General Electric Company. Atomic Power Equipment Department (page images at HathiTrust)
A study of feedback, blade and hub parameters on flap bending due to non-uniform rotor-disk turbulence (Southern Illinois University at Edwardsville, Dept. of Mathematical Studies, 1976), by G. H. Gaonkar and A. K. Subramanian (page images at HathiTrust; US access only)
Additional measurements of the drag of surface irregularities in turbulent boundary layers (NACA, 1951), by W. Tillmann and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
Some lagrangian properties of turbulence deduced from atmospheric diffusion (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1966., 1966), by Duane A. Haugen and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
The influence of correlation time of fluctuation fields on the stochastic growth of water droplets (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1968., 1968), by Wen Ching-Sung and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Vertical profiles of wind speeds from measurements of high towers (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1968., 1968), by M. M. Borisenko, M. V. Zavarina, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
The turbulence in quiescent prominences and shock waves in the upper atmosphere (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1970., 1970), by E. Ye Dubov and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Dynamics and structure of the quiet thermosphere (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1974), by K. S. W. Champion and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Plasma heating through parametrically induced turbulence (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratories, Air Force Systems Command, United States Air Force, 1976., 1976), by Arthur Lawrence Pavel and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
A study of turbulent flow in rough pipes (Univ. of Illinois, 1965), by James M. Robertson, John David Martin, and Thomas Henry Burkhart (page images at HathiTrust; US access only)
A review of experimental data of vertical turbulent buoyant jets (Iowa Institute of Hydraulic Research, University of Iowa, 1976), by Ching Jen Chen and Wolfgang Rodi (page images at HathiTrust; US access only)
The relation of turbulance to diffusion in open-channel flows (U.S. Dept. of the Interior, Geological Survey, Water Resources Division, 1971), by Thomas N. Keefer (page images at HathiTrust)
On some general features of turbulent flows with large Reynolds numbers (Brookhaven National Laboratory, Dept. of Nuclear Energy, Nuclear Waste Research Group;, 1982), by Arnold Levin and Brookhaven National Laboratory. Atmospheric Sciences Division (page images at HathiTrust)
Kansas 1968 field program data report (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1971), by Yutaka Izumi and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
A Method for determining the point of lift-off and modified trajectory of a ground-based heated turbulent planar jet in a co-flowing wind (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), by Milton M. Klein and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
Atmospheric properties from measurements at Kwajalein Atoll on 5 April 1978 (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1978., 1978), by C. R. Philbrick, B. W. Kennedy, R. O. Olsen, D. W. Blood, J. E. Salah, T. Hanrahan, E. T. Jr Fletcher, J. P. Noonan, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
The diurnal variation of turbopause height (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1980., 1980), by S. P. Zimmerman and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
Joint agency turbulence experiment interim report (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1983., 1983), by Alan R. Bohne and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
On the difference between waves and turbulence in a stratified fluid (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratories, Air Force Systems Command, United States Air Force, 1982., 1982), by Edmond M. Dewan and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
Modelling turbulence in the lower atmosphere using Richardson's criterion (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1981., 1981), by Edmund A. Murphy, Kathryn G. Scharr, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
Some characteristics of turbulence at high altitudes (Bedford, Massachusetts : Atmospheric Circulations Laboratory, Geophysics Research Directorate, Air Forece Cambridge Research Center, 1958., 1958), by Mariano A. Estoque and Air Force Cambridge Research Laboratories (U.S.). Atmospheric Circulations Laboratory (page images at HathiTrust)
The rotor flow in the lee of mountains (Bedford, Massachusetts : Meteorological Development Laboratory, Geophysics Research Directorate, Air Force Cambridge Research Center, 1959., 1959), by Joachim P. Kuettner and Air Force Cambridge Research Center (U.S.). Geophysics Research Directorate (page images at HathiTrust)
A diffusion-deposition model For in-flight release of fission fragments (Bedford, Massachusetts : Geophysics Research Directorate, Air Force Cambridge Research Center, Air Research and Development Command, United States Air Force, 1960., 1960), by M. L.; Barad, J. J. Fuquay, D. A. Haugen, and Air Force Cambridge Research Center (U.S.). Geophysics Research Directorate (page images at HathiTrust)
Turbulent diffusion in liquid jets. (For sale by the Supt. of Docs., U.S. Govt. Print. Off., 1974), by Strong C. Chaung, Victor W. Goldschmidt, Warren S. Stevenson, Charles H. Tinsley, and United States. Environmental Protection Agency. Office of Research and Development (page images at HathiTrust; US access only)
Turbulence-- : its causes and effects (Washington, D.C. : U.S. G.P.O., [1955], 1955), by United States. Weather Bureau (page images at HathiTrust)
The mountain wave-- : what it means to the pilot (Washington, D.C. : U.S. G.P.O., 1955., 1955), by United States. Weather Bureau (page images at HathiTrust)
Mountain winds and their effects on flight (Washington, D.C. : Civil Aeronautics Board, Bureau of Safety Investigation : U.S. G.P.O., 1951., 1951), by George M. French and United States. Civil Aeronautics Board. Bureau of Safety Investigation (page images at HathiTrust)
Keep your distance ([Washington, D.C.] : [Civil Aeronautics Board, Bureau of Safety Investigation] : U.S. Government Printing Office, 1953., 1953), by Harold G. Crowley, R. W. Chrisp, and United States. Civil Aeronautics Board. Bureau of Safety Investigation (page images at HathiTrust)
Turbulent nonbuoyant or buoyant jets discharged into flowing or quiescent fluids (Iowa Institute of Hydraulic Research, University of Iowa, 1972), by Tzeng-Long Chan, J. F. Kennedy, United States. Office of Naval Research, and Marley Company (page images at HathiTrust; US access only)
Propagation of density disturbances in air-water flow (Evanston, Ill., 1965), by George Peter Nassos (page images at HathiTrust)
The Graetz problem in cocurrent-flow, double-pipe, heat exchangers (Argonne National Laboratory, Reactor Engineering Division, 1964), by Ralph P. Stein and Argonne National Laboratory (page images at HathiTrust)
A method of calculating transient temperatures in a multiregion, axisymmetric, cylindrical configuration, the ARGUS program, 1089/RE248, written in FORTRAN II (Argonne National Laboratory, Reactor Physics Division, 1963), by D. F. Schoeberle, L. B. Miller, J. Heestand, and Argonne National Laboratory (page images at HathiTrust)
Study of effects of turbulence promoters on heat transfer (Oak Ridge, Tennessee : Fairchild Engine and Airplane Corporation, NEPA Division 1950., 1950), by Armour Research Foundation (U.S.), Andrew H. Dowdy, Fairchild Engine and Airplane Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust)
Preliminary measurements of atmospheric turbulence at high altitude as determined from acceleration measurements on Lockheed U-2 airplane (National Advisory Committee for Aeronautics, 1957), by Thomas L. Coleman, Jack Funk, and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
Airplane measurements of atmospheric turbulence for altitudes between 20,000 and 55,000 feet over the Western part of the United States (National Advisory Committee for Aeronautics, 1957), by Thomas L. Coleman, Emilie C. Coe, and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
Local isotropy in turbulent shear flow (National Advisory Committee for Aeronautics, 1958), by Stanley Corrsin and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
On the application and interpretation of coherent motion detectors (1991), by Charles Paul Gendrich (page images at HathiTrust; US access only)
Turbulence and Reynolds stress distribution in a natural river (U.S. Fish and Wildlife Service, Environmental Management Technical Center, 1993), by Bijoy S. Mazumder, Ta Wei Soong, Nani G. Bhowmik, and Environmental Management Technical Center (U.S.) (page images at HathiTrust)
Annual research briefs ... (NASA, Ames Research Center ;, in the 20th century), by Center for Turbulence Research (U.S.), Stanford University, and Ames Research Center (page images at HathiTrust)
Theoretical studies of the mixing process of a jet impinging into a stream of large mass (University of Illinois, Aeronautical Engineering Dept., 1955), by Illinois. University. Dept. of Aeronautical Engineering, H. S. Stillwell, and T. P. Torda (page images at HathiTrust; US access only)
On turbulent fluid motion (Hydrodynamics Laboratory, California Institute of Technology, 1951), by J. M. Burgers (page images at HathiTrust; US access only)
Compressible turbulent skin friction on rough and rough/wavy walls in adiabatic flow. (Silver Spring, Maryland : Naval Ordnance Laboratory, White Oak, 1974., 1974), by Daniel C. Reda and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
A Study of the effect of pressure gradient on the eddy viscosity and mixing length for incompressible equilibrium turbulent boundary layers (Silver Spring, Maryland : Naval Ordnance Laboratory, 1974., 1974), by W. J. Glowacki, S. W. Chi, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Comparisons of experiment with a general equation for the coagulation of heterogeneous aerosols. ([Canoga Park, California] : Atomics International, North American Rockwell, 1969., 1969), by M. A. Greenfield, D. H. Hausknecht, R. L. Koontz, U.S. Atomic Energy Commission, and Rockwell International. Atomics International Division (page images at HathiTrust)
Turbulent eddies in high-density-spark channels in helium (L. G. Hansom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1967., 1967), by Heinz Fischer, Karlheinz Sch©·onbach, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
An Experimental study of the effects of non-uniform wall temperature on heat transfer in laminar and turbulent axisymmetric flow along a cylinder (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by R. Eichhorn, A. D. Anderson, E. R. G. Eckert, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
Gust loading of rigid and flexible aircraft in continuous atmospheric turbulence (Wright Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by Kenneth A. Foss, Warren L. McCabe, United States. Air Force. Air Research and Development Command, and Wright Air Development Center (page images at HathiTrust)
Simplified procedures for the calculation of heat transfer to surfaces with non-uniform temperatures (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1956., 1956), by J. P. Hartnett, R. L. Sampson, Roland Birkebak, E. R. G. Eckert, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and University of Minnesota. Department of Mechanical Engineering. Heat Transfer Laboratory (page images at HathiTrust)
Inhibition of flow separation at high speed. Volume 1, Supersonic turbulent boundary layers (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1969., 1969), by Larry L. Lynes, Frederick K. Goodwin, Jack Norman Nielsen, Air Force Flight Dynamics Laboratory (U.S.), and Nielsen Engineering & Research (page images at HathiTrust)
An investigation of laminar, transitional and turbulent heat transfer on blunt-nosed bodies in hypersonic flow (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), by Robert J. Cresci, Paul A. Libby, Donald A. MacKenzie, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Polytechnic Institute of Brooklyn. |b Department of Aerospace Engineering and Applied Mechanics (page images at HathiTrust)
Derivation of sufficient conditions for application of the distorted-wave born approximation to turbulent wake backscatter (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1974), by Ronald L. Fante and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Turbulent heat transfer on blunt-nosed bodies in two-dimensional and general three-dimensional hypersonic flow (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1958., 1958), by Roberto Vaglio-Laurin, United States. Air Force. Air Research and Development Command, Wright Air Development Center, and Polytechnic Institute of Brooklyn. Department of Aeronautical Engineering and Applied Mechanics (page images at HathiTrust)
Further studies on high-speed unsteady flow (Wright-Patterson Air Force Systems Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Garabed Zartarian, Harry Sauerwein, United States. Air Force. Systems Command. Aeronautical Systems Division, and Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory (page images at HathiTrust)
Exact vorticity solutions of the incompressible Navier-Stokes equations (L.G. Hansom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1970., 1970), by Harry E. Moses and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
On the imaging of incoherent objects in a turbulent medium (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1975), by Ronald L. Fante and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Radar cross section of underdense turbulent wakes (Air Force Cambridge Research Laboratories, Air Force System Command, United States Air Force, 1973), by Ronald L. Fante and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
B-66B low level gust study. Volume XI, Crew Comments. Part 2, Flights G-54-G115 (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Flight Dynamics Laboratory, Air Research and Development Command, United States Air Force, 1961., 1961), by Air Force Flight Dynamics Laboratory (U.S.), United States. Wright Air Development Division, United States. Air Force. Air Research and Development Command, and Douglas Aircraft Company (page images at HathiTrust)
Response of aircraft encountering aircraft wake turbulence (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), by Robert C. Nelson and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Medium altitude critical atmospheric turbulence (MEDCAT) data processing and analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), by J. P. Ryan, Kurt C. Rolle, Robert J. Dominic, A. C. Robertson, A. P. Berens, Air Force Flight Dynamics Laboratory (U.S.), and University of Dayton. Research Institute (page images at HathiTrust)
Optimal large eddy simulation of turbulence (Arlington, Virginia : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 2004., 2004), by Robert deLancey Moser, R. J. Adrian, S. Balachandar, University of Illinois at Urbana-Champaign. Department of Theoretical and Applied Mechanics, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Study of mixing and reaction in the field of a vortex (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, United States Air Force, 1987., 1987), by B. M. Cetegen, W. A. Sirignano, Irvine. Department of Mechanical Engineering University of California, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Calculation of skin friction intwo-dimensional, transonic, turbulent flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1979., 1979), by T. W. Swafford, Inc ARO, United States. Air Force. Arnold Air Force Base, and Arnold Engineering Development Center (page images at HathiTrust)
Integrated microtransducer and neural networks system for distributed control (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, 1998., 1998), by Chih-Ming Ho, Los Angeles. Mechanical University of California, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Large eddy and unstructured grid methods for heat transfer applications in propulsion systems (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, 1998., 1998), by Richard H. Pletcher, Iowa State University. Department of Mechanical Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Evaluation of closure models of turbulent diffusion flames (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 2000., 2000), by G. Kosaly, James J. Riley, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
An investigation of ducted, two-stream, variable-density, turbulent jet mixing with recirculation (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1977., 1977), by Roy J. Schulz, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
A Study of turbulent boundary layer structure (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, United States Air Force, 1986., 1986), by John L. Lumley, Cornell University, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Contractors' meeting in turbulence and rotating flows (Arlington, Virginia : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1999., 1999), by Thomas Beutner and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Investigation of the turbulence producing structures in the boundary layer (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1991., 1991), by S. J. Kline, Stanford University. Thermosciences Division, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Propagation of electromagnetic waves through turbulent media using transport theory (L.G. Hanscom Field, Massachusetts : Air Force Cambridge Research Laboratories, Air Force System Command, United States Air Force, 1972., 1972), by Ronald L. Fante and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Advancing detached eddy simulation (Arlington, Virginia. : Air Force Office of Scientific Research, 2007., 2007), by Kyle D. Squires, Arizona State University. Department of Mechanical and Aerospace Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Theoretical and experimental investigation of flow over single and double backward facing steps ([Washington, D.C.] : [United States Air Force, Office of Scientific Research], [1961], 1961), by Douglas Eugene Abbott, S. J. Kline, United States. Air Force. Office of Scientific Research, and Stanford University. Department of Mechanical Engineering (page images at HathiTrust)
Analytical nodel of supersonic, turbulent, near-wake flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1976., 1976), by C. E. Peters, W. J. Phares, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
Developing new generation of models for turbulent flows (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, United States Air Force, 1997., 1997), by Katepalli R. Sreenivasan, United States. Air Force. Office of Scientific Research, and Yale University. Department of Engineering and Applied Science (page images at HathiTrust)
Second moment closure modeling of complex turbulent flows (Arlington, Virginia. : Air Force Office of Scientific Research, 2007., 2007), by Sharath Girimaji, Lawrence Ukeiley, Mark N. Glauser, Jeremy T. Pinier, Texas A & M University. Aerospace Engineering Department, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Investigation of turbulent jet impingement in a confined crossflow (Wright-Patterson Air Force Base, Ohio : Fliight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, 1991, 1991), by George D. Catalano, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, and La.). Department of Mechanical Engineering Louisiana State University (Baton Rouge (page images at HathiTrust)
Fundamental aspects of the structure of supersonic turbulent boundary layers (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, United States Air Force, 1988., 1988), by Alexander J. Smits, Princeton University. Department of Mechanical and Aerospace Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Large eddy simulation of turbulent flow over an airfoil using unstructured grids (Arlington, Virginia. : Air Force Office of Scientific Research, 1999., 1999), by Kenneth E. Jansen, Aeronautical Engineering Rensselaer Polytechnic Institute. Mechanical Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Parallel multigrid DNS/LES methods for time-dependent turbulent flow (Arlington, Virginia : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 2003., 2003), by Chaoqun Liu, University of Texas at Arlington. Department of Mathematics, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
An analytical and experimental study of the plane, incompressible, turbulent free shear layer with arbitrary velocity ratio and pressure gradient (Stanford, California : Department of Mechanical Engineering, Stanford University, 1963., 1963), by C. M. Sabin, Stanford University. Department of Mechanical Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Chemical reactions in turbulent mixing flows (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, 1998., 1998), by Paul E. Dimotakis, Anthony Leonard, California Institute of Technology. Graduate Aeronautical Laboratories, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Experimental study of the turbulence production mechanism in boundary layer flows (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1982., 1982), by R. E. Falco, Michigan State University. Department of Mechanical Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Active feedback interaction with a shear layer (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1987., 1987), by Paul E. Dimotakis, M. M. Koochesfahani, California Institute of Technology. Graduate Aeronautical Laboratories, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Optimal controller for turbulent flow over an airfoil (Arlington, Virginia. : Air Force Office of Scientific Research, 2006., 2006), by John Kim, Los Angeles. Mechanical University of California, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
On three-dimensional free-mixing ([Washington, D.C.] : [United States Air Force, Office of Scientific Research], [1960], 1960), by Martin H. Bloom, United States. Air Force. Office of Scientific Research, and Polytechnic Institute of Brooklyn. Department of Aeronautical Engineering and Applied Mechanics (page images at HathiTrust)
Active feedback interaction with a shear layer (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, United States Air Force, 1986., 1986), by Paul E. Dimotakis, M. M. Koochesfahani, Daniel Guggenheim Aeronautical Laboratory, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
The effect of pressure pulsations and vibrations on fully developed pipe flow (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1981., 1981), by Donald O. Barnett, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
Structure based turbulence modeling (Arlington, Virginia : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 2004., 2004), by William C. Reynolds, Carlos A. Langer, Stavros Kassinos, Stanford University. Department of Mechanical Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Coherent structure reflective turbulent viscous flow modeling (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1987., 1987), by Gustave J. Hokenson and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
(U) Physical models for supersonic turbulent boundary layer structure (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1989., 1989), by Alexander J. Smits, Princeton University. Gas Dynamics Laboratory, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Interaction of isotropic turbulence with a shock wave (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1992., 1992), by S. Lee, S. K. Lele, Parviz Moin, Stanford University. Thermosciences Division, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Turbulence modeling (Ithaca, New York : Cornell University, Sibley School of Mechanical and Aerospace Engineering, 1994., 1994), by John L. Lumley, Sibley School of Mechanical and Aerospace Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Stagnation point flow and heat transfer under free-stream turbulence (Arlington, Virginia : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 2004., 2004), by Zhongmin Xiong, Sanjiva K. Lele, Stanford University. Department of Mechanical Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
The compressible turbulent boundary layer with surface mass transfer ([Washington, D.C.] : [United States Air Force, Office of Scientific Research], [1960], 1960), by F. Culick, United States. Air Force. Office of Scientific Research, and Massachusetts Institute of Technology. Naval Supersonic Laboratory (page images at HathiTrust)
Boundary layer transition at supersonic speeds : three dimensional roughness effects (spheres) (Washington, D.C. : Air Force Office of Scientific Research, United States Air Force, 1961., 1961), by E. R. Van Driest, C. B. Blumer, United States. Air Force. Office of Scientific Research, and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
Interaction of chemistry, turbulence and shock waves in hypervelocity flow (Pasadena, California : California Institute of Technology, 1994., 1994), by G. V. Candler, B. Sturtevant, D. Pullin, B. V. McKoy, D. Meiron, A. Leonard, H. Hornung, P. Dimotakis, California Institute of Technology, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
An experimental investigation of the flow structure of the turbulent boundary layer (Stanford, California : Department of Mechanical Engineering, Stanford University, 1963., 1963), by Peter W. Runstadler, William C. Reynolds, S. J. Kline, Stanford University. Department of Mechanical Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Studies on the structure of turbulence (Cambridge, Massachusetts : Geophysics Research Directorate, Air Force Cambridge Research Center, Air Research and Development Command, United States Air Force, 1958., 1958), by J. A. Businger, Hans A. Panofsky, Verner Suomi, University of Wisconsin. Department of Meteorology, and Air Force Cambridge Research Center (U.S.). Geophysics Research Directorate (page images at HathiTrust)
Some measurements of a wake-boundary layer interaction (Wright-Patterson Air Force Base, Ohio : Aeronautical Research Laboratories, Air Force Research Division, Air Research and Development Command, United States Air Force, 1960., 1960), by R. Eichhorn, T. L. Eddy, United States. Air Force. Aeronautical Research Laboratories, and University of Minnesota (page images at HathiTrust)
Parallel multi-scale algorithms and applications to turbulence (Bolling Air Force Base, D.C. : AFOSR/NM, 1997., 1997), by George E. Karniadakis, Brown University. Division of Applied Mathematics, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Dynamic structure LES models (Arlington, Virginia : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 2005., 2005), by Christopher J. Rutland, University of Wisconsin--Madison. Engine Research Center, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Turbulent reacting flows at high speed (Princeton New Jersey : Princeton University, 1996., 1996), by Alexander J. Smits, J. Fielding, F. L. Dryer, Princeton University, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Large eddy simulation of turbulent combustion (Arlington, Virginia. : Air Force Office of Scientific Research, 2006., 2006), by Heinz Pitsch, Daniel Kirk, Hector Guiterrez, Stanford University, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Point heat sources and the temperature-vorticity analogy in compressible boundary layers (Washington, D.C. : Air Force Office of Scientific Research, United States Air Force, 1962., 1962), by W. J. McCroskey, United States. Air Force. Office of Scientific Research, and Princeton University. Department of Aeronautical Engineering (page images at HathiTrust)
Laminar, transitional, and turbulent heat transfer measurements on a yawed blunt conical nosetip (Los Angeles, California : Space and Missile Systems Organization, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1972., 1972), by George F. Widhopf, United States. Air Force. Systems Command, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
Compressible turbulent reacting flows (Arlington, Virginia : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 2000., 2000), by F. A. Williams, Shondeep L. Sarkar, Paul A. Libby, San Diego University of California, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Structure-based turbulence model (Stanford, California : Stanford University, Department of Mechanical Engineering, 1995., 1995), by William C. Reynolds, Stanford University. Department of Mechanical Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Receiver noise due to R/V plasma sheath turbulence (L.G. Hanscom Field, Massachusetts : Air Force Cambridge Research Laboratories, Air Force System Command, United States Air Force, 1972., 1972), by Ronald L. Fante and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Turbulence and complex flow phenomena in multi-stage axial turbomachines (Arlington, Virginia. : Air Force Office of Scientific Research, 2007., 2007), by Joseph Katz, Charles Meneveau, Johns Hopkins University, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Subsonic free turbulent shear flow (Stanford, California : Thermosciences Division, Department of Mechanical Engineering, Stanford University, 1964., 1964), by R. M. Halleen, Stanford University. Department of Mechanical Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Management and control of unsteady and turbulent flows (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, United States Air Force, 1988., 1988), by Hassan M. Nagib, David R. Williams, John L Way, Candace E. Wark, Patrick H. Reisenthel, Thomas C. Corke, Mukund Acharya, Illinois Institute of Technology. Department of Mechanical and Aerospace Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
A Final report on three-dimensional structure of transitional boundary layers (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1990., 1990), by W. S. Saric, Arizona State University. Department of Mechanical and Aerospace Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Simulation of turbulent hypersonic flows : subgrid-scale model for the temperature fluctuations in reacting turbulence (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, 1997., 1997), by Graham V. Candler, M. Pino Martin, University of Minnesota. Department of Aerospace Engineering and Mechanics, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
An experimental study of the receptivity of a compressible laminar boundary layer (Arlington, Virginia. : Air Force Office of Scientific Research, 2008., 2008), by Garry L. Brown, Hadassah Naiman, Princeton University, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Studies of hypersonic boundary layer behavior (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1995., 1995), by A. J. Smits, G. L. Brown, R. B. Miles, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Vorticity-stream function formulation of compressible and incompressible turbulent internal flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1979., 1979), by John C. Chien, Inc ARO, United States. Air Force. Arnold Air Force Base, and Arnold Engineering Development Center (page images at HathiTrust)
Compressible flow turbulence simulation and modeling via additive turbulent decomposition (Lexington, Kentucky : University of Kentucky, 1996., 1996), by J. M. McDonough, University of Kentucky, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
A visual study of the flow model in the later stages of laminar-turbulent transition on a flat plate (Stanford, California : Stanford University, Department of Mechanical Engineering, 1961., 1961), by C. A. Meyer, S. J. Kline, United States. Air Force. Office of Scientific Research, and Stanford University. Department of Mechanical Engineering (page images at HathiTrust)
Mutual coherence function of a beam propagating in a turbulent medium (L.G. Hanscom Field, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973., 1973), by Ronald L. Fante and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Receptivity in boundary-layer transition to turbulence (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, United States Air Force, 1996., 1996), by W. S. Saric, United States. Air Force. Office of Scientific Research, and Arizona State University. College of Engineering and Applied Sciences (page images at HathiTrust)
Chemical reactions in turbulent mixing flows (Pasadena, California : California Institute of Technology, Firestone Flight Sciences Laboratory, Guggenheim Aeronautical Laboratory, Karman Laboratory of Fluid Mechanics and Jet Propulsion, 1995., 1995), by Paul E. Dimotakis, Anthony Leonard, United States. Air Force. Office of Scientific Research, and Daniel Guggenheim Aeronautical Laboratory (page images at HathiTrust)
Interaction of chemistry, turbulence, and shock waves in hypervelocity flow (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, 1999., 1999), by Graham V. Candler, B. Sturtevant, D. I. Pullin, B. V. McKoy, Daniel I. Meiron, Anthony Leonard, H. G. Hornung, Paul E. Dimotakis, Daniel Guggenheim Aeronautical Laboratory, California Institute of Technology. Graduate Aeronautical Laboratories, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Numerical analysis of recirculating ducted flows (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1978., 1978), by R. J. Schulz, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
Proceedings of the AFFDL/NASA/FAA wake turbulence workshop : 4-5 June 1974. (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Control Criteria Branch, Flight Control Division, Stability and Control Group, Air Force Systems Command, United States Air Force, 1975., 1974), by F. L. Paillet and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
Wind tunnel investigation of a spike-bluff body combination for a monorail rocket sled M = 2.0 to M = 5.0 (Holloman Air Force Base, New Mexico : Air Force Office of Scientific Research, Directorate of Research Analyses, United States Air Force, 1962., 1962), by Rudolf Hermann, Donald Olson, Frederick Moynihan, United States. Air Force. Office of Scientific Research, Rosemount Aeronautical Laboratories, and University of Minnesota. Institute of Technology (page images at HathiTrust)
The Heat transfer and fluid dynamics of concave surface curvature (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1988., 1988), by P. Bradshaw, R. L. Moffat, J. P. Johnston, Stanford University. Department of Mechanical Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Integrated computational/experimental study of turbulence modification and mixing enhancement in swirling jets (Arlington, Virginia. : Air Force Office of Scientific Research, 2009., 2009), by Jonathan W. Naughton, C. Zemtsop, M. Stoellinger, Richard Semaan, S. Heinz, Dan Stanescu, University of Wyoming. Mechanical Engineering Department, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
An experimental investigation of ducted, reactive, turbulent jet mixing with recirculation. (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Engine Test Facility, Air Force Systems Command, United States Air Force, 1977., 1977), by D. E. Chriss, United States. Air Force. Systems Command, Arnold Engineering Development Center, and Inc ARO (page images at HathiTrust)
Large eddy simulation for heat transfer prediction in a gas turbine environment : development of a high-order overset mesh LES solver (Arlington, Virginia. : Air Force Office of Scientific Research, 2007., 2007), by Sanjiva K. Lele, Zhongmin Xiong, Rathakrishnan Bhaskaran, Stanford University. Department of Mechanical Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Influence of turbulence on surface reaeration (University of Illinois Water Resources Center, 1966), by Edward R. Holley, K. K. Klintworth, and United States. Office of Water Resources Research (page images at HathiTrust; US access only)
Laminar, transitional, and turbulent heat transfer to a cone-cylinder-flare body at Mach 8.0 (Air Force Office of Scientific Research, United States Air Force, 1962), by Victor Zakkay, Clifton J. Callahan, Polytechnic Institute of Brooklyn. Dept. of Aerospace Engineering and Applied Mechanics, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
Towards understanding turbulent scalar mixing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Sharath S. Girimaji and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
Convective storm downdraft outflows detected by NASA/MSFC's airborne 10.6 [micro]m pulsed Doppler lidar system (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by G. D. Emmitt and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Probability density functions in turbulent channel flow (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Surya P. G. Dinavahi, United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, and Langley Research Center (page images at HathiTrust)
A structured fluids approach to canopy flow (New York University, 1970), by Mark N. Silbert (page images at HathiTrust)
Development of a near-wall Reynolds-stress closure based on the SSG model for the pressure strain (National Aeronautics and Space Administration, Langley Research Center, 1994), by R. M. C. So and Langley Research Center (page images at HathiTrust)
Horizontal diffusion from an instantaneous point-source due to oceanic turbulence (Chesapeake Bay Institute, Johns Hopkins University, 1962), by Akira Ōkubo, U.S. Atomic Energy Commission, and Chesapeake Bay Institute (page images at HathiTrust; US access only)
Experimental study of vane heat transfer and aerodynamics at elevated levels of turbulence (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1994), by Forrest E. Ames and Lewis Research Center (page images at HathiTrust)
Experimental investigation of flow-induced cavity resonance (West Bethesda, Maryland : Signatures Directorate, Naval Surface Warfare Center, Carderock Division, 2000., 2000), by Paul Zoccola and Naval Surface Warfare Center (U.S.). Carderock Division (page images at HathiTrust)
An experimental study of the turbulent wake behind a cone at Mach 5 (White Oak, Maryland : United States Naval Ordnance Laboratory, 1966., 1966), by William C. Ragsdale and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
A laboratory investigation into flight path perturbations during steep descents of V/STOL aircraft (Wright-Patterson AFB, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1976), by L. D. Reid, Peter C. Hughes, H. W. Teunissen, Bernard Etkin, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command, and University of Toronto. Institute for Aerospace Studies (page images at HathiTrust)
Current marks on firm mud bottoms (New Haven, 1962), by Stanisław Dżułyński and John E. Sanders (page images at HathiTrust; US access only)

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