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Turbulent boundary layer

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• Boundary layer
• Turbulence

• Calculation of compressible turbulent boundary layers with pressure gradients and heat transfer / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by Larry L. Lynes, Gary D. Kuhn, Jack Norman Nielsen, Nielsen Engineering & Research, and Ames Research Center (page images at HathiTrust)
• Engineering prediction of turbulent skin friction and heat transfer in high-speed flow / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Aubrey M. Cary, Mitchel H. Bertram, and Langley Research Center (page images at HathiTrust)
• Approximate formulas for the computation of turbulent boundary-layer momentum thicknesses in compressible flows / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1946), by Neal Tetervin, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• The boundary layers in fluids with little friction : = Grenzschichten in flüssigkeiten mit kleiner reibung / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by H. Blasius and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Heat transmission in the boundary layer / (Washington, D.C. : NACA, 1949), by L. E. |q Kalikhman and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the recording of turbulent longitudinal and transverse fluctuations / (Washington, D.C. : NACA, 1951), by Helmut Reichardt and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the theory of the turbulent boundary layer / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Julius C. Rotta and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Calculation of turbulent expansion processes / (Washington, D.C. : NACA, 1945), by Walter Tollmien and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• On the contribution of turbulent boundary layers to the noise inside a fuselage / (Washington, D.C. : NACA, 1956), by G. M. Corcos, H. W. Liepmann, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Representation of turbulent shear stress by a product of mean velocity differences / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Willis H. Braun and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A general model of the ocean mixed layer : using a two-component turbulent kinetic energy budget with mean turbulent field closure / (Seattle, Wash. : Dept. of Commerce, National Oceanic and Atmospheric Administration, Environmental Research Laboratories, Pacific Marine Environmental Laboratory, 1976), by Roland W. Garwood, Pacific Marine Environmental Laboratory (U.S.), and Environmental Research Laboratories (U.S.) (page images at HathiTrust)
• Numerical investigation of separated transonic turbulent flows with a multiple-time-scale turbulence model ([Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 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)
• Flight transition data for angles of attack at Mach 22 with correlations of the data / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Charles B. Johnson, Christine M. Darden, and Langley Research Center (page images at HathiTrust)
• An investigation of the high speed turbulent boundary layer with heat transfer and arbitrary pressure gradient / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1970), by Constantino Economos, J. L. Boccio, Langley Research Center, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Calculation of turbulent boundary layers with heat transfer and pressure gradient utilizing a compressibility transformation. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by J. Boccio, C. Economos, Langley Research Center, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Supersonic turbulent boundary-layer flows with mass injection through slots and/or porous walls / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1975), by Alvin L. Murray, Langley Research Center, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Turbulent fluid friction of rotating disks / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by P. Cooper, Lewis Research Center, and Case Western Reserve University (page images at HathiTrust)
• A finite-difference method for predicting supersonic turbulent boundary-layer flows with tangential slot injection / (Washington, D.C. : National Aeronautics and Space Administration, [1972]), by E. W. Miner, C. H. Lewis, Langley Research Center, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• An experimental investigation of vortex generation in a turbulent boundary layer undergoing adverse pressure gradient / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Victor Zakkay, Wladimiro Calarese, Langley Research Center, and New York University (page images at HathiTrust)
• An experimental study of slot injection into a supersonic stream / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Michael Kenworthy, Joseph A. Schetz, Langley Research Center, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Thin radiating shock layer about a blunt body / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by Y. S. Chou, L. H. Blake, Ames Research Center, and Lockheed Aircraft Corporation (page images at HathiTrust)
• Analytical and experimental investigation of circulation control by means of a turbulent Coanda jet / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by E. S. Levinsky, T. T. Yeh, Ames Research Center, and Air Vehicle Corporation (page images at HathiTrust)
• Effects of Mach number on pitot-probe displacment in a turbulent boundary layer / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Jerry M. Allen and Langley Research Center (page images at HathiTrust)
• Fluctuating pressures measured beneath a high-temperature, turbulent boundary layer on a flat plate at a Mach number of 5 / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by Tony L. Parrott, Cindy W. Albertson, Michael G. Jones, and Langley Research Center (page images at HathiTrust)
• Unified analysis of turbulent jet mixing / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by Joseph A. Schetz, Johns Hopkins University, University of Maryland at College Park, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of variable property turbulent boundary layers by means of a modified compressibility transformation / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by C. Economos, J. L. Boccio, Langley Research Center, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Computer program for calculating laminar and turbulent boundary layer development in compressible flow / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by H. J. Herring, G. L. Mellor, Lewis Research Center, and Princeton University (page images at HathiTrust)
• Differential analysis for the turbulent boundary layer on a compressor blade element (including boundary-layer separation) / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by James F. Schmidt, Carroll A. Todd, and Lewis Research Center (page images at HathiTrust)
• Data on effects of incident-reflecting shocks on the turbulent boundary layer / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by S. Z. Pinckney and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Calculation of compressible, nonadiabatic boundary layers in laminar, transitional and turbulent flow by the method of integral relations / (Washington, D.C. : National Aeronautics and Space Administration, 1971), by Gary D. Kuhn, United States. National Aeronautical and Space Administration, Nielsen Engineering & Research, and Langley Research Center (page images at HathiTrust)
• Calculation of turbulent boundary layers with heat transfer and pressure gradient utilizing a compressibility transformation. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1971), by C. Economos, J. Boccio, Langley Research Center, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Calculation of turbulent boundary layers with heat transfer and pressure gradient utilizing a compressibility transformation. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by J. Schneider, J. Boccio, Langley Research Center, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Parametric study of relaminarization of turbulent boundary layers on nozzle walls / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by J. P. Kreskovsky, H. McDonald, S. J. Shamroth, Langley Research Center, and United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
• The calculation of three-dimensional turbulent boundary layers on helicopter rotors / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by J. G. Hicks, J. F. Nash, Lockheed-Georgia Company, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Analysis of laminar flow between stationary and rotating disks with inflow / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by Upendra S. Rohatgi, Eli Reshotko, Lewis Research Center, and Case Western Reserve University (page images at HathiTrust)
• Relaxation of an unsteady turbulent boundary layer on a flat plate in an expansion tube / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Roop N. Gupta, Robert L. Trimpi, and Langley Research Center (page images at HathiTrust)
• Computer program for calculating laminar, transitional, and turbulent boundary layers for a compressible axisymmetric flow / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by James A. Albers, John L. Gregg, and Lewis Research Center (page images at HathiTrust)
• Laminar or turbulent boundary-layer flows of perfect gases or reacting gas mixtures in chemical equilibrium / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1971), by E. Clay Anderson, Clark H. Lewis, Langley Research Center, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• FORTRAN program for calculating compressible laminar and turbulent boundary layers in arbitrary pressure gradients / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970), by William D. McNally (page images at HathiTrust)
• The compressible turbulent boundary layer on a blunt swept slab with and without leading-edge blowing / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1971), by James L. Hunt, Ivan E. Beckwith, Dennis M. Bushnell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of a turbulent boundary layer over a moving ground plane / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Alan T. Roper, Garl L. Gentry, and Langley Research Center (page images at HathiTrust)
• Pitot-probe displacement in a supersonic turbulent boundary layer (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1972), by Jerry M. Allen, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Interference heating from interactions of shock waves with turbulent boundary layers at Mach 6 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Charles B. Johnson, Louis G. Kaufman, and Langley Research Center (page images at HathiTrust)
• Effects of spiral longitudinal vortices on turbulent boundary layer skin friction / ([Washington] : National Aeronautics and Space Administration, [1964]), by J. G. Spangler, C. S. Wells, Ling-Temco-Vought, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Turbulent heat-transfer prediction method for application to scramjet engines / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by S. Z. Pinckney and Langley Research Center (page images at HathiTrust)
• Theoretical face pressure and drag characteristics of forward-facing steps in supersonic turbulent boundary layers / (Washington : National Aeronautics and Space Administration, 1975), by D. K. Patel and K. R. Czarnecki (page images at HathiTrust)
• Analysis of an existing experiment on the interaction of acoustic waves with a laminar boundary layer / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by M. R. Schopper, Langley Research Center, Systems and Applied Sciences Corporation, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Turbulent boundary layer heat transfer experiments : convex curvature effects including introduction and recovery / (Washington. D.C. National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by T. W. Simon, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Drag of two-dimensional small-amplitude symmetric and asymmetric wavy walls in turbulent boundary layers / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by John C. Lin, R. Balasubramanian, Michael J. Walsh, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Exploratory investigation of the effect of porous surfaces on hypersonic turbulent boundary layers / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by Ralph D. Watson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Turbulent boundary layers over nonstationary plane boundaries / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Office, 1978), by Alan T. Roper, Garl L. Gentry, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Turbulent boundary layer over solid and porous surfaces with small roughness / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Fred Y. Kong, Fayette Collier, Joseph A. Schetz, Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Dept, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• M=3 turbulent boundary layer measurements at very high Reynolds numbers / (Wright-Patterson Air Force Base : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1977), by Anthony W. Fiore (page images at HathiTrust)
• Turbulent boundary-layer separation induced by flares on cylinders at zero angle of attack / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Supt. of Docs., U.S. G.P.O., Washington 25, D.C. 22151], 1961), by Donald M. Kuehn and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Base pressure coefficients obtained from the X-15 airplane for Mach numbers up to 6 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia], 1964), by Edwin J. Saltzman, United States National Aeronautics and Space Administration, and Flight Research Center (U.S.) (page images at HathiTrust; US access only)
• Power-law velocity-profile-exponent variations with Reynolds number, wall cooling, and Mach number in a turbulent boundary layer / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 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)
• Investigation of laminar and turbulent boundary layers interacting with externally generated shock waves / (Washington : National Aeronautics and Space Administration, 1969), by Earl C. Watson, William C. Rose, and John D. Murphy (page images at HathiTrust; US access only)
• Some turbulent boundary-layer measurements obtained from the forebody of an airplane at Mach numbers up to 1.72 / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Edwin J. Saltzman, David F. Fisher, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Excitation of boundary-layer turbulence through spark discharges / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Enrique J. Klein, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Compressible turbulent boundary layers; a symposium held at Langley Research Center, Hampton, Virginia, December 10-11, 1968. (Washington, Scientific and Technical Information Division, National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1969), by Langley Research Center (page images at HathiTrust; US access only)
• Additional measurements of the drag of surface irregularities in turbulent boundary layers / (Washington : NACA, 1951), by W. Tillmann 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)
• Thick axisymmetric turbulent boundary layer and near wake of a low-drag body of revolution / (Iowa City : Iowa Institute of Hydraulic Research, University of Iowa, [1977]), by V. C. Patel, Y. T. Lee, Iowa State Water Resources Research Institute, and David W. Taylor Naval Ship Research and Development Center (page images at HathiTrust; US access only)
• On the equations of a thick axisymmetric turbulent boundary layer / (Iowa City : Institute of Hydraulic Research, University of Iowa, [1973]), by V. C. Patel, Iowa Institute of Hydraulic Research, and Naval Ship Research and Development Center (page images at HathiTrust; US access only)
• A unified view of the law of the wall using mixing-length theory / (Iowa City : Institute of Hydraulic Research, University of Iowa, 1972), by Virandrakumar Chaturbhai Patel and Naval Ship Research and Development Center (page images at HathiTrust; US access only)
• Proceedings of the Aero-Optics Symposium on Electromagnetic Wave Propagation from Aircraft, held at Ames Research Center, Moffett Field, California, August 14-15, 1979 / (Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : for sale by the National Technical Information Service], 1980), by Calif.) Aero-Optics Symposium on Electromagnetic Wave Propagation from Aircraft (1979 : Moffett Field, Ames Research Center, and Air Force Weapons Laboratory (page images at HathiTrust)
• Calculation of the turbulent boundary layer and of transition on a plane plate, ([Washington] National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., [1968, i.e. 1967]), by René Hirsch (page images at HathiTrust; US access only)
• Numerical solution of the equations for compressible laminar, transitional, and turbulent boundary layers and comparisons with experimental data / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1971), by Julius E. Harris, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Turbulent-boundary-layer heat-transfer and transition measurements with surface cooling at Mach 6 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va. 22151], 1970), by Aubrey M. Cary, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Power- and cross-spectra and space-time correlations of surface fluctuating pressures at Mach numbers between 1.6 and 2.5 / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va. 22151], 1969), by Wei J. Chyu, Richard D. Hanly, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Pressure fluctuations in turbulent boundary layers / (Washington, D.C. : National Aeronautics and Space Administration, 1965), by M. V. Lowson, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Experimental investigation of the turbulent boundary layer at a Mach number of 6 with heat transfer at high Reynolds numbers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1967), by Richard D. Samuels, Jerry B. Adcock, John B. Peterson, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Investigation of small surface protuberances upstream of turbulent boundary layer separation produced by a skewed shock wave at Mach 3 / (Wright-Patterson Air Force Base, Ohio : Air Force Aero Propulsion Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Syspems Command, 1976), by Robert H Korkegi and Air Force Aero Propulsion Laboratory (U.S.) Ramjet Technology Branch (page images at HathiTrust)
• Flight-measured pressure characteristics of aft-facing steps in high Reyonlds number flow at Mach numbers of 2.20, 2.50, and 2.80 and comparison with other data / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Office, 1978), by Sheryll Goecke Powers and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Computer program for solving laminar, transitional, or turbulent compressible boundary-layer equations for two-dimensional and axisymmetric flow / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Julius E. Harris, Doris K. Blanchard, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Control of shock wave - boundary layer interactions by bleed in supersonic mixed compression inlets / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Michael K. Fukuda, Eli Reshotko, Warren R. Hingst, Lewis Research Center, and Case Western Reserve University (page images at HathiTrust)
• A computational model for the prediction of jet entrainment in the vicinity of nozzle boattails (The BOAT code) / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Service ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Sanford M. Dash, Harold S. Pergament, Aeronautical Research Associates of Princeton, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Simulation of turbulent wall pressure / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Information Service, 1978), by Robert L. Ash, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Semiempirical method for predicting effects of incident-reflecting shocks on the turbulent boundary layer / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1965]), by S. Z. Pinckney and Langley Research Center (page images at HathiTrust)
• Pressure and heat-transfer distributions in a simulated wing-elevon cove with variable leakage at a free-stream Mach number of 6.9 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1978), by William D. Deveikis, Whitney Bartlett, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A potential-flow/boundary layer method for calculating subsonic and transonic airfoil flow with trailing-edge separation / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Richard W. Barnwell, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Evaluation of analytical procedures for prediction of turbulent boundary layers on a porous wall / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Charles E. Towne and Lewis Research Center (page images at HathiTrust)
• Three-dimensional turbulent-mixing-length modeling for discrete-hole coolant injection into a crossflow / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 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)
• Comparison of several methods for predicting separation in a compressible turbulent boundary layer / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Philip M. Gerhart, Lawrence J. Bober, and Lewis Research Center (page images at HathiTrust)
• Calculation of the pressure distribution on axisymmetric boattails including effects of viscous interactions and exhaust jets in subsonic flow / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Josef Rom, Lawrence J. Bober, and Lewis Research Center (page images at HathiTrust)
• Methods for estimating pressure and thermal loads induced by elevon deflections on hypersonic-vehicle surfaces with turbulent boundary layers / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Louis G. Kàufman, Charles B. Johnson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Experimental evaluation of compliant surfaces at low speeds / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Kenneth W. McAlister, Tom M. Wynn, U.S. Army Air Mobility Research and Development Laboratory, and Ames Research Center (page images at HathiTrust)
• Characteristics of Mach 10 transitional and turbulent boundary layers / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Ralph D. Watson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Turbulent-flow separation criteria for overexpanded supersonic nozzles / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by E. Leon Morrisette, Theodore J. Goldberg, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Mean-flow and turbulence measurements in the vicinity of the trailing edge of an NACA 63₁-012 airfoil / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by James C. Yu, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Aerothermal environment in chordwise gaps between split elevons at Mach 6.8 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by L. Roane Hunt, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Robert D. Quinn, Leslie Gong, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Flight test results of a trailing edge flap designed for direct-lift control / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by Charles R. Taylor, Boeing Company, and Ames Research Center (page images at HathiTrust)
• Skin friction reduction in supersonic flow by injection through slots, porous sections and combinations of the two / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, [1975]), by Joseph A. Schetz, Johannes VanOvereem, Langley Research Center, and Virginia Polytechnic Institute and State University (page images at HathiTrust)
• Prediction of compliant wall drag reduction, part I / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Steven A. Orszag, inc Cambridge Hydrodynamics, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A study of surface pressure fluctuations in hypersonic turbulent boundary layers / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1974]), by K. R. Raman, Ames Research Center, and Nielsen Engineering & Research (page images at HathiTrust)
• On the theory of compliant wall drag reduction in turbulent boundary layers / (Washington, D.C. : National Aeronautics and Space Administration, 1974), by Robert L. Ash, Langley Research Center, and Old Dominion University (page images at HathiTrust)
• Use of multiple discrete wall jets for delaying boundary layer separation / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1974]), by J. D. McLean, H. J. Herring, Lewis Research Center, and Princeton University (page images at HathiTrust)
• Further studies of unsteady boundary layers with flow reversal / (Washington : U.S. National Aeronautics and Space Administration;, 1976), by John F. Nash, Ames Research Center, and inc Sybucon (page images at HathiTrust)
• Finite element analysis of low speed viscous and inviscid aerodynamic flows / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by A. J. Baker and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental investigation of shock wave-turbulent boundary layer interactions with and without boundary layer suction : a data summary report / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Chen-Chih Sun, Morris E. Childs, and University of Washington (page images at HathiTrust)
• A low speed two-dimensional study of flow separation on the GA(W)-1 airfoil with 30-percent chord Fowler flap / (Washington, D.C. : National Aeronautics and Space Administration, [1977]), by H. C. Seetharam, W. H. Wentz, Wichita State University, and Langley Research Center (page images at HathiTrust)
• Experimental and theoretical investigation of three-dimensional turbulent boundary layers and turbulence characteristics inside an axial flow inducer passage / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by A. K. Anand, B. Lakshminarayana, Pennsylvania State University, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A Computer program to calculate incompressible laminar and turbulent boundary layer development / (Washington, D.C. : National Aeronautics and Space Administration, 1970), by H. J. Herring, G. L. Mellor, United States National Aeronautics and Space Administration, Lewis Research Center, and Princeton University (page images at HathiTrust)
• Transitional boundary-layer solutions using a mixing-length and a two-equation turbulence model / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by E. Clay Anderson, David C. Wilcox, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Operational manual for two-dimensional transonic code TSFOIL / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Stephen S. Stahara, Ames Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Nielsen Engineering & Research (page images at HathiTrust)
• A visual investigation of turbulence in stagnation flow about a circular cylinder / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Willy Z. Sadeh, Herbert J. Brauer, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Colorado State University (page images at HathiTrust)
• Finite-difference solution of the compressible stability eigenvalue problem / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Mujeeb R. Malik, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Systems and Applied Sciences Corporation, and Langley Research Center (page images at HathiTrust)
• Interaction between a normal shock wave and a turbulent boundary layer at high, transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Thomas Charles Adamson, Arthur F. Messiter, M. S. Liou, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Transition fixing for hypersonic flow / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by James R. Sterrett and Langley Research Center (page images at HathiTrust)
• Experimental laminar, transitional, and turbulent boundary-layer profiles on a wedge at local Mach number 6.5 and comparisons with theory / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Michael C. Fischer, Dal V. Maddalon, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of the influence of the turbulent boundary layer on the pressure distribution over a rigid two-dimensional wavy wall / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1971]), by Lado Muhlstein, Richard G. Beranek, George C. Marshall Space Flight Center, and Ames Research Center (page images at HathiTrust)
• Comparisons of turbulent-boundary-layer measurements at Mach number 19.5 with theory and an assessment of probe errors [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Ivan E. Beckwith, Frank L. Clark, William D. Harvey, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat-transfer measurements at a Mach number of 2 in the turbulent boundary layer on a flat plate having a stepwise temperature distribution / (Washington : National Aeronautics and Space Administration, [1959]), by Raul J. Conti and Langley Research Center (page images at HathiTrust)
• Investigation by Schlieren technique of methods of fixing fully turbulent flow on models at supersonic speeds / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Mary W. Jackson, K. R. Czarnecki, and Langley Research Center (page images at HathiTrust)
• Experimental separation studies for two-dimensional wedges and curved surfaces at Mach numbers of 4.8 to 6.2 / (Washington : National Aeronautics and Space Administration, [1962]), by James R. Sterrett, James C. Emery, and Langley Research Center (page images at HathiTrust)
• Free flight observation of a separated turbulent flow including heat transfer up to Mach 8.5 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Dudley George McConnell and Lewis Research Center (page images at HathiTrust)
• Similar solutions for turbulent boundary layer with large favorble pressures gradients (nozzle flow with heat transfer) / (Washington : National Aeronautics and Space Administration, 1971), by James F. Schmidt, Carroll Todd, Donald R. Boldman, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Heat transfer and boundary layer in conical nozzles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972), by Donald R. Boldman, Robert W. Graham, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Prediction of local and integrated heat transfer in nozzles using an integral turbulent boundary layer / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972), by Donald R. Boldman, Robert C. Ehlers, James F. Schmidt, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Some characteristics of turbulent boundary layers in rapidly accelerated flows / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Paul F. Brinich, Harvey E. Neumann, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Elizabeth B. Plentovich, M. B. Tracy, and Julio Chu (page images at HathiTrust)
• An experimental investigation of turbulent boundary layers along curved surfaces / (Washington, D.C. : National Aeronautics and Space Administration, [1972]), by Ronald M. C. So, George L. Mellor, Lewis Research Center, and Princeton University (page images at HathiTrust)
• Skin friction reduction by slot injection at mach 0.8 / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Victor Zakkay, Chi R. Wang, United States National Aeronautics and Space Administration, Langley Research Center, and New York University (page images at HathiTrust)
• Flowfield analysis for successive oblique shock wave-turbulent boundary layer interactions / (Washington : National Aeronautics and Space Administration, Ames Research Center ;, 1976), by Chen-Chih Sun, Morris E. Childs, and Washington State University. Dept. of Mechanical Engineering (page images at HathiTrust)
• Atmospheric flow over two-dimensional bluff surface obstructions / (Washington : National Aeronautics and Space Administration, 1976), by Juergen Bitte, Walter Frost, George C. Marshall Space Flight Center, and University of Tennessee (Knoxville campus). Space Institute (page images at HathiTrust)
• Calculation of laminar and turbulent boundary layers for two-dimensional time-dependent flows / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Tuncer Cebeci, Long Beach California State University, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of blown boundary layers with an improved wall jet system / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by K. R. Saripalli, R. L. Simpson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Measurements of laminar and turbulent flow in a curved duct with thin inlet boundary layers / (Washington, D.C. National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by A. M. K. P. Taylor, M. Yianneskis, James H. Whitelaw, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Interference drag in a simulated wing-fuselage juncture / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by L. Kubendran, J. Hubbartt, H. McMahon, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• A Three-dimensional turbulent compressible subsonic duct flow analysis for use with constructed coordinate systems / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by R. Levy, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Scaling and modeling of three-dimensional, end-wall, turbulent boundary layers / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1984), by Uriel C. Goldberg, Eli Reshotko, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Case Western Reserve University, and Lewis Research Center (page images at HathiTrust)
• Mean velocities and Reynolds stresses in a juncture flow / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by H. McMahon, J. Hubbartt, L. Kubendran, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Georgia Institute of Technology, and Langley Research Center (page images at HathiTrust)
• Flow separation in shock wave boundary layer interactions at hypersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by A. Hamed, Langley Research Center, and Joint Institute for Advancement of Flight Sciences (page images at HathiTrust)
• A transonic interactive boundary-layer theory for laminar and turbulent flow over swept wings / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by Shawn H. Woodson, Fred R. DeJarnette, and Langley Research Center (page images at HathiTrust)
• Unsteady motion of a wing of finite span in a compressible medium / (Washington : National Aeronautics and Space Administration, 1961), by E. A. Krasilʹshchikova (page images at HathiTrust)
• Systematic study of error sources in supersonic skin-friction balance measurements / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Jerry M. Allen, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Velocity, intermittency, and turbulence intensity measurements in the boundary layer of an accelerated flow / (Washington, D.C. : National Aeronautics and Space Administration, 1970), by Donald R. Boldman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Further experimental results on the influence of the turbulent boundary layer on panel flutter / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Peter A. Gaspers, Daniel N. Petroff, Lado Muhlstein, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical study of reactive and nonreactive turbulent coaxial jets / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Roop N. Gupta, N. T. Wakelyn, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance and boundary-layer evaluation of a sonic inlet / (Washington : National Aeronautics and Space Administration ;, 1976), by James F. Schmidt, Robert S. Ruggeri, and Lewis Research Center (page images at HathiTrust)
• Comparison of prediction methods and studies of relaxation in hypersonic turbulent nozzle-wall boundary layers / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va. 22151], 1969), by Dennis M. Bushnell, William V. Feller, William D. Harvey, Charles B. Johnson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Downstream influence of swept slot injection in hypersonic turbulent flow / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Jerry N. Hefner, Dennis M. Bushnell, Aubrey M. Carey, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Fluctuating properties of turbulent boundary layers for Mach numbers up to 9 / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by William D. Harvey, Ivan E. Beckwith, Dennis M. Bushnell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Penetration model explanation for turbulent forced-convection heat transfer observed in near-critical fluids / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969]), by Robert W. Graham, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Summary of available information on Reynolds analogy for zero-pressure-gradient, compressible, turbulent-boundary-layer flow / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970]), by Aubrey M. Cary, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Preliminary surveys of the wall boundary layer in a Mach 6 axisymmetric tunnel / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970]), by Robert A. Jones, William V. Feller, and Langley Research Center (page images at HathiTrust)
• Starting phenomena for hypersonic inlets with thick turbulent boundary layers at Mach 6 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Theodore J. Goldberg, Jerry N. Hefner, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Accuracy of pitot-pressure rakes for turbulent boundary-layer measurements in supersonic flow / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1971), by Earl R. Keener, Edward J. Hopkins, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Evaluation of mean and turbulent velocity measurements in subsonic accelerated boundary layers / (Washington : National Aeronautics and Space Administration ;, 1976), by V. A. Sandborn, H. L. Seegmiller, and Ames Research Center (page images at HathiTrust)
• Flow visualization by elastic light scattering in the boundary layer of a supersonic flow / (Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, 2000), by G. C. Herring, Mervin E. Hillard, and Langley Research Center (page images at HathiTrust)
• Flow-field measurements downstream of two protuberances on a flat plate submerged in a turbulent boundary layer at Mach 2.49 and 4.44 / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Lana M. Couch, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Evaluation of boundary-layer and wake-survey data-reduction techniques in compressible flows / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by K. R. Czarnecki, Russell B. Sorrells, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Drag reduction due to gas injection through various discrete slots on a three-dimensional wing at Mach 2.01 / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1969), by Russell B. Sorrells, Lorraine F. Satchell, K. R. Czarnecki, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• A method of calculating compressible turbulent boundary layers / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by H. James Herring and George L. Mellor (page images at HathiTrust; US access only)
• Turbulent boundary layers in adverse pressure gradients /, by Francis H. Clauser and Johns Hopkins University. Department of Aeronautics (page images at HathiTrust; US access only)
• Narrow band cross-correlation analysis of fluctuating pressures beneath a turbulent boundary layer / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by C. M. Ailman and A. S. Hopkins (page images at HathiTrust; US access only)
• Spectra and space-time correlations of the fluctuating pressures at a wall beneath a supersonic turbulent boundary layer perturbed by steps and shock waves / (Washington, D.C. : National Aeronautics and Space Administration, 1966), by W. V. Speaker (page images at HathiTrust; US access only)
• An analytical study of the measured wall pressure field under supersonic turbulent boundary layers / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by Thomas J. Black (page images at HathiTrust; US access only)
• An aircraft investigation of turbulence in the lower layers of a marine boundary layer /, by Robert Louis Grossman, B. R. Bean, and Environmental Research Laboratories (U.S.) (page images at HathiTrust)
• Laminarization of a turbulent boundary layer as observed from heat-transfer and boundary-layer measurements in conical nozzles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Donald R. Boldman, Anne K. Gallagher, James F. Schmidt, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Detailed description and results of a method for computing mean and fluctuating quantities in turbulent boundary layers / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Ivan E. Beckwith, Dennis M. Bushnell, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Eddy viscosities and mixing lengths for turbulent boundary layers on flat plates, smooth or rough / (Bethesda, MD : David W. Taylor Naval Ship Research and Development Center, [1986]), by Paul S. Granville and David W. Taylor Naval Ship Research and Development Center (page images at HathiTrust)
• Big eddies and mixing processes in the Great Lakes / (Washington, D.C. : U.S. Environmental Protection Agency, Office of Research and Development : For sale by the Supt. of Docs., U.S. Govt. Print. Off., 1973), by G. T. Csanady and United States. Environmental Protection Agency. Office of Research and Development (page images at HathiTrust)
• Mixing-length formulations for turbulent boundary layers over arbitrarily rough surfaces / (Bethesda, Md. : 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)
• Supersonic mixing of jets and turbulent boundary layers /, by Harry E. Bailey, Arnold M. Kuethe, United States. Air Force. Air Research and Development Command. sponsor, and Wright Air Development Center (page images at HathiTrust)
• Measurements of aerodynamic heat transfer in turbulent separated regions at a Mach number of 1.8 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by Benjamine J. Garland, J. R. Hall, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Approximate turbulent boundary-layer development in plane compressible flow along thermally insulated surfaces with application to supersonic-tunnel contour correction / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by Maurice Tucker and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Investigation of separation of the turbulent boundary layer / (Washington, D.C. : 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)
• An exploratory theoretical investigation of the effect of longitudinal surface curvature on the turbulent boundary layer /, by Neal Tetervin and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Velocity profile, skin-friction balance and heat-transfer measurements of the turbulent boundary layers at Mach 5 and zero-pressure gradient /, by Roland E. Lee, A. C. Leonas, William Joseph Yanta, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Investigation of substructure heating on cracked ablative heat shields /, by Erhard M Winkler, M. T. Madden, J. A. Koenig, Richard L. Humphrey, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Supersonic ablation studies with teflon /, by Erhard M Winkler, J. A. Koenig, Richard L. Humphrey, M. T. Madden, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Flow visualization studies of a fin protuberance partially Immersed in a turbulent boundary layer at mach 5 /, by Allen E. Winkelmann and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Drag of several surface protrusion patterns at M = 5.0 /, by John A. Darling and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Measurements of a mach 4.9 zero-pressure-gradient turbulent boundary layer with heat yransfer., by Robert L. P. Voisinet, Roland E. Lee, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Measurements of a supersonic favorable-pressure-gradient turbulent boundary layer with heat Transfer : part 1 -data compilation. /, by Robert L. P. Voisinet, Roland E. Lee, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Comparative measurements of total temperature in a supersonic turbulent boundary layer using a conical equilibrium and combined temperature-pressure probe. /, by R. L. P. Voisinet, H. U. Meier, Roland E. Lee, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Compressible turbulent skin friction on rough and rough/wavy walls in adiabatic flow. /, by Daniel C Reda and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Analytical procedures used to obtain and evaluate the eddy viscosity and mixing length extracted from incompressible turbulent boundary layer data /, by W. J. Glowacki 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 /, by W. J. Glowacki, S. W. Chi, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• On the motions of particles in turbulent flows / (Washington, D.C. : The Commission : Available from GPO Sales Program, Division of Technical Information and Document Control, U.S. Nuclear Regulatory Commission ; Springfield, Va. : National Technical Information Service, 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)
• Experimental convective heat transfer to a 4-inch and 6-inch hemisphere at Mach numbers from 1.62 to 3.04 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Leo T. Chauvin, Joseph P. Maloney, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Normal force, center of pressure, and zero-lift drag of several ballistic-type missiles at Mach numbers of 4.05 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Edward F. Ulmann, Robert W. Dunning, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Measurements in the boundary layer of a yawed wing / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by A. M. Kuethe, W. H. Curry, P. B. McKee, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Turbulent boundary-layer temperature recovery factors in two-dimensional supersonic flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Maurice Tucker, Stephen H. Maslen, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Characteristics of turbulence in a boundary layer with zero pressure gradient / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by P. S. Klebanoff and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• The Nature and variability of integrated boundary layer winds / (L.G. Hanscom Field, Bedford, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1974), by René V. Cormier and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Fluctuation measurements in supersonic turbulent boundary layers /, by Alan. L. Kistler and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• Measurements of hypersonic turbulent heat transfer on a highly cooled cone /, by Donald M Wilson and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• An analytical investigation of the flat plate turbulent boundary layer in compressible flow /, by Neal Tetervin and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• A digital computer program for making comparative aerodynamic heat transfer and skin friction drag calculations /, by Donald M Wilson and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• An approximate method for the calculation of the reynolds analogy factor for a compressible turbulent boundary layer in a pressure gradient /, by Neal Tetervin and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• An experimental investigation of the surface Pitot probe including effects of heat transfer and compressibility /, by David L. Brott, Roland E. Lee, William Joseph Yanta, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• A generalization to turbulent boundary layers of Mangler's transformation between axisymmetric and two-dimensional laminar boundary layers /, by Neal Tetervin and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• A correlation of heat-transfer and skin-friction data and an experimental Reynolds analogy factor for highly cooled turbulent boundary layers at Mach 5.0 /, by Donald M Wilson and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Hypersonic-turbulent boundary-layer separation over a cone-cylinder-flare configuration /, by Arnold Polak, Chris A. Kalivretenos, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• An experimental investigation of the compressible turbulent boundary layer with a favorable pressure gradient /, by David L. Brott, Roland E. Lee, Robert L. Voisinet, William Joseph Yanta, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Two-dimensional jet interaction with a mach 4 mainstream /, by Michael J Werle, David G. Shaffer, Richard T. Driftmyer, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• The prediction of turbulent boundary-layer separation Influenced by blowing /, by Arnold Polak and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Calculation of magnus forces on axisymmetric bodies at small angles of attack with incompressible turbulent boundary layers /, by Neal Tetervin and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• A forward facing step study: the step height less than the boundary-layer thickness /, by Richard T. Driftmyer and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Measurements of upstream history effects in compressible turbulent boundary layers /, by David F Gates and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• A magnus theory for bodies of revolution /, by H. R. Vaughn, G. E. Reis, Sandia Corporation, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Interacting supersonic turbulent boundary layers over a two-dimensional protuberance. /, by Arnold Polak and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Calculation of high speed inlet flows using the Navier-Stokes equations., by Doyle D. Knight, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Rutgers University. Department of Mechanical & Aerospace Engineering (page images at HathiTrust)
• High speed flow separation ahead of finite span steps /, by Louis G. Kaufman, Robert D. Kirchner, sponsor Air Force Flight Dynamics Laboratory (U.S.), and issuing body United States. Air Force. Systems Command (page images at HathiTrust)
• Skin friction measurements at a Mach number of three and momentum thickness Reynolds numbers up to a half million /, by Anthony W. Fiore and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• An automated procedure for computing the three-dimensional transonic flow over wing-body combinations, including viscous effects., by William H. Mason, Juanita Frick, W. F. Ballhaus, Mark Stern, Donald Mackenzie, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Grumman Aerospace Corporation, and issuing body United States. Air Force. Systems Command (page images at HathiTrust)
• Heat transfer and flow with separated and reattached boundary layers as produced by surface irregularities /, by R. A. Seban, Berkeley. Institute of Engineering Research University of California, and Wright Air Development Center issuing body (page images at HathiTrust)
• Boundary layer effects : proceedings of the 7th U.S. Air Force/Federal Republic of Germany Data Exchange Agreement Meeting /, by Anthony W. Fiore, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Germany (West), sponsor United States. Air Force, and Ohio) U.S. Air Force/Federal Republic of Germany Data Exchange Agreement Meeting (7th : 1978 : Wright Patterson Air Force Base (page images at HathiTrust)
• Prediction of pressure fuctuations associated with maneuvering re-entry weapons., by Anthony L. Laganelli, John R. Howe, sponsor Air Force Flight Dynamics Laboratory (U.S.), issuing body United States. Air Force. Systems Command, and sponsor General Electric Company. Re-entry and Environmental Systems Division (page images at HathiTrust)
• The effects of artificial stimulation of the turbulent boundary layer in rectangular conduits. (Vicksburg, Miss. : Waterways Experiment Station, 1956), by Waterways Experiment Station (U.S.) (page images at HathiTrust)
• Finite span effects on flap heating and effectiveness in a turbulent boundary layer /, by L. A. Cassel, S. Taylor, L. D. McMillen, sponsor Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and inc. Science Applications (page images at HathiTrust)
• Mark IV supersonic-hypsersonic arbitrary-body program modifications and computer graphics., by S. Taylor, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Air Force Wright Aeronautical Laboratories, and inc. Science Applications (page images at HathiTrust)
• Viscous and interacting flow field effects : proceedings of the 9th U.S. Air Force and the Federal Republic of Germany Data Exchange Agreement Meeting /, by Md.) U.S. Air Force/Federal Republic of Germany Data Exchange Agreement Meeting (9th : 1984 : Silver Springs, Anthony W. Fiore, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Critical evaluation of transition from laminar to turbulent shear layers with emphasis on hypersonically traveling bodies /, by Mark Vladimir Morkovin, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and Md.) Research Institute for Advanced Study (Baltimore (page images at HathiTrust)
• Inhibition of flow separation at high speed., by Larry L. Lynes, Frederick K. Goodwin, Jack Norman Nielsen, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Nielsen Engineering & Research (page images at HathiTrust)
• Mark IV supersonic-hypsersonic arbitrary-body program modifications and computer graphics., by S. Taylor, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Air Force Wright Aeronautical Laboratories, and inc. Science Applications (page images at HathiTrust)
• Flight text investigation of transonic shock-boundary layer phenomena /, by Jones F. Cahill, Bill L. Copper, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-Georgia Company (page images at HathiTrust)
• Study of the effect of free-stream turbulence upon disturbances in the pre-transitional laminar boundary layer /, by James M. Kendall, sponsor Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Jet Propulsion Laboratory (U.S.) (page images at HathiTrust)
• Turbulent boundary layer flow over a flat plate vibrating with transverse standing waves / (Minneapolis : University of Minnesota, St. Anthony Falls Hydraulic Laboratory, 1962), by Albert G. Mercer and St. Anthony Falls Hydraulic Laboratory (page images at HathiTrust; US access only)
• Pressure gradient effects on supersonic boundary layer turbulence : final report /, by A. J. Laderman, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Ford Aerospace & Communications Corporation. Fluid Mechanics Section (page images at HathiTrust)
• Dominance of radiated aerodynamic noise on boundary-layer transition in supersonic-hypersonic wind tunnels : theory and application /, by Samuel R. Pate, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Separated and nonseparated turbulent flows about axisymmetric nozzle afterbodies., by John A. Benek, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Advancing detached eddy simulation /, by Kyle D. Squires, sponsor Arizona State University. Department of Mechanical and Aerospace Engineering, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Effects of acoustic and vortical disturbances on the turbulent boundary layer at free-stream Mach number 0.5 /, by John A. Benek, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• An Improved interaction method for calculating exhaust nozzle boattail flows /, by Gary D. Kuhn, United States. Air Force. Arnold Air Force Base. sponsor, Arnold Engineering Development Center. sponsor, and Nielsen Engineering & Research. issuing body (page images at HathiTrust)
• A Method of calculating turbulent-boundary-layer growth at hypersonic Mach numbers /, by James C. Sivells, Robert G. Payne, Inc. sponsor ARO, United States. Air Force. Arnold Air Force Base. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• Analytical description of the complete two-dimensional turbulent boundary-layer velocity profile /, by David L. Whitfield, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Wall models for large-eddy simulation based on optimal control theory /, by Parviz Moin, Meng Wang, Jeremy A. Templeton, sponsor Stanford University. Department of Mechanical Engineering, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Integral analysis of ducted two-stream mixing with recirculation /, by C. E. Peters, W. J. Phares, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Integral solution of compressible turbulent boundary layers using improved velocity profiles /, by David L. Whitfield, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Critical sting length as determined by the measurement of pitch-damping derivatives for laminar, transitional, and turbulent boundary layers at Mach number 3 for reduced frequencies of 0.0033 and 0.0056 /, by Bob L. Uselton, Fred B. Cyran, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Holographic interferometry measurements of subsonic turbulent boundary layers /, by D. W. Sinclair, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Analytical approximation of two-dimensional separated turbulent boundary-layer velocity profiles /, by T. W. Swafford, R. K. Matthews, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Stability and transition analysis for reentry tool, STAR /, by Helen L. Reed, sponsor Texas A & M University. Aerospace Engineering Department, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Analysis of the three-dimensional compressible turbulent boundary layer on a sharp cone at incidence in supersonic and hypersonic flow /, by John C. Adams, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• A robust scheme for control of skin friction and heat transfer in turbulent boundary layers via new instability mechanism /, by Fazle Hussain, Wade Schoppa, sponsor University of Houston. Department of Mechanical Engineering, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Stability theory for cross hatching., by Lester Lees, Asher Sigal, T. Kubota, issuing body United States. Air Force. Systems Command, sponsor Space and Missile Systems Organization (U.S.), and sponsor California Institute of Technology (page images at HathiTrust)
• Stability theory for cross hatching., by Lester Lees, Denny R. S. Ko, T. Kubota, issuing body United States. Air Force. Systems Command, sponsor Space and Missile Systems Organization (U.S.), and sponsor California Institute of Technology (page images at HathiTrust)
• Fundamental studies of subsonic and transonic flow separation., by J. M. Wu, K. Anjaneyulu, Herbert Venghaus, L. Shen, R. Nygaard, C. H. Chen, K. C. Reddy, G. M. Elfstrom, Trevor H. Moulden, University of Tennessee (System). Space Institute. sponsor, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Evaluation of a method for computation of separated, turbulent, compressible boundary layers /, by M. C. Altstatt, Arnold Engineering Development Center. sponsor, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Noise generation in transonic wind tunnels /, by M. O. Varner, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Wall temperature effects on two- and three-dimensional transonic turbulent boundary layers /, by J. C Adams, Arloe W Mayne, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Analytical, numerical, and experimental results on turbulent boundary layers /, by David L. Whitfield, Arnold Engineering Development Center. sponsor, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Uniform roughness studies /, by David E. Klett, M. Kithcart, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor North Carolina Agricultural and Technical State University, and sponsor Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
• Shock wave - turbulent boundary layer interaction in high speed flow /, by Michael S. Holden, issuing body Aerospace Research Laboratories (U.S.), and sponsor Calspan Corporation (page images at HathiTrust)
• Effects of mass transfer into laminar and turbulent boundary layers over cones at angle of attack /, by Michael C. Frieders, United States. Air Force. Systems Command. Arnold Engineering Development Center. sponsor, and Virginia Polytechnic Institute and State University. issuing body (page images at HathiTrust)
• Investigation of the physics of screech in supersonic jets and turbulent boundary layers at high Reynolds number and control of separation through oscillatory blowing /, by Hassan M. Nagib, Michael Hites, I. Wygnanski, Ahmed Naguib, Candace Wark, issuing body United States. Air Force. Office of Scientific Research, and sponsor Illinois Institute of Technology (page images at HathiTrust)
• Prediction of turbulent skin friction for two-dimensional, rib-type surface roughness using a discrete element approach /, by Robert P. Taylor, Hugh W. Coleman, B. K. Hodge, issuing body Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Rockwell International (page images at HathiTrust)
• Wing pressure distribution and boundary layer data obtained from C-5A flight testing /, by Jones F. Cahill, William A. Stevens, issuing body Aerospace Research Laboratories (U.S.), and sponsor Lockheed-Georgia Company (page images at HathiTrust)
• Research on supersonic turbulent separated and reattached flows /, by Seymour M. Bogdonoff, G. Simpers, G. S. Settles, Irwin E. Vas, issuing body Aerospace Research Laboratories (U.S.), and sponsor Princeton University. Gas Dynamics Laboratory (page images at HathiTrust)
• Numerical study of separated turbulent flows /, by David C. Wilcox, issuing body Aerospace Research Laboratories (U.S.), and sponsor United States. National Technical Information Service (page images at HathiTrust)
• Fundamental studies of subsonic and transonic flow separation., by J. M. Wu, United States. Air Force. Systems Command. Arnold Engineering Development Center. sponsor, and University of Tennessee (System). Space Institute. issuing body (page images at HathiTrust)
• Two-dimensional compression corner and planar shock wave interactions with a supersonic, turbulent boundary layer /, by C. Herbert Law, issuing body Aerospace Research Laboratories (U.S.), and Aerospace Research Laboratories (U.S.). Theoretical Aerodynamics Research Laboratory (page images at HathiTrust)
• Three-dimensional turbulent boundary layers /, by O. Sendstad, Parviz Moin, Stanford University. Stanford University. Thermosciences Division sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Developing new generation of models for turbulent flows /, by Katepalli R. Sreenivasan, issuing body United States. Air Force. Office of Scientific Research, and sponsor Yale University. Department of Engineering and Applied Science (page images at HathiTrust)
• An analytical and experimental study of the plane, incompressible, turbulent free shear layer with arbitrary velocity ratio and pressure gradient /, by C. M. Sabin, sponsor Stanford University. Department of Mechanical Engineering, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Control of separation for turbulent boundary layers subjected to wall curvature and streamwise pressure gradients /, by Hermann F. Fasel, University of Arizona. Department of Aerospace and Mechanical Engineering. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Flow transition in gas turbine airfoil boundary layers: fundamentals and empiricisms /, by Gregory S. West, Lit S. Han, issuing body Air Force Wright Aeronautical Laboratories, and sponsor University of Dayton. Research Institute (page images at HathiTrust)
• Wave evolution and laminar-turbulent transition in fully 3D supersonic flows /, by T. Herbert and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• An experimental investigation of the flow structure of the turbulent boundary layer /, by Peter W. Runstadler, William C. Reynolds, S. J. Kline, sponsor Stanford University. Department of Mechanical Engineering, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Transition in high-speed boundary layers : numerical investigations using DNS and LES /, by Hermann F. Fasel, University of Arizona. Department of Aerospace and Mechanical Engineering. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Investigation of supersonic boundary layer transition and turbulent structure /, by Alexander J. Smits, R. B. Miles, Princeton University. Gas Dynamics Laboratory. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Boundary layer transition and surface roughness effects in hypersonic flow /, by Michael S. Holden, Calspan Corporation. Advanced Technology Center. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Turbulent boundary layer characteristics at high Reynolds number /, by V. Zakkay, issuing body Aerospace Research Laboratories (U.S.), and sponsor New York University. Aerospace and Energetics Laboratory (page images at HathiTrust)
• Experiments on the interaction with a turbulent boundary layer of a skewed shock wave of variable strength at mach 2.5 /, by L. Michael Freeman, Robert H. Korkegi, and issuing body Aerospace Research Laboratories (U.S.) (page images at HathiTrust)
• Fundamental studies of subsonic and transonic flow separation., by Zhengming Wu, United States. Air Force. Systems Command. Arnold Engineering Development Center. sponsor, and University of Tennessee (System). Space Institute. issuing body (page images at HathiTrust)
• Three-dimensional shock wave-turbulent boundary layer interactions at Mach 6 /, by C. Herbert Law and issuing body Aerospace Research Laboratories (U.S.) (page images at HathiTrust)
• Controlled experiments on instabilities and transition to turbulence on elliptic cones at hypersonic mach numbers /, by Thomas C. Corke, University of Notre Dame. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Viscous flow interaction studies : final report on work unit 7064 02 06 /, by Robert H. Korkegi and issuing body Aerospace Research Laboratories (U.S.) (page images at HathiTrust)
• Two-dimensional turbulent boundary layer separation on a flat plate with ramp at freestream Mach numbers of 3.7 and 6.3 in supersonic and hypersonic flow /, by V. Zakkay, issuing body Aerospace Research Laboratories (U.S.), and sponsor New York University. Aerospace and Energetics Laboratory (page images at HathiTrust)
• Theoretical investigation of 3-D shock wave-turbulent boundary layer interactions : part VII /, by Doyle D. Knight, United States. Air Force. Office of Scientific Research. issuing body, and Rutgers University. Department of Mechanical & Aerospace Engineering. sponsor (page images at HathiTrust)
• A Method for computing boundary-layer flows, including normal pressure gradient and longitudinal curvature effects /, by Arloe W. Mayne, United States. Air Force. Arnold Air Force Base. sponsor, United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body, and Inc. sponsor ARO (page images at HathiTrust)
• Parametric study of hypersonic turbulent boundary layers with heat transfer /, by J. S. Shang, issuing body Aerospace Research Laboratories (U.S.), and sponsor Hypersonic Research Laboratory (U.S.) (page images at HathiTrust)
• Numerical study of a three-dimensional turbulent boundary layer /, by Parviz Moin, United States. Air Force. Office of Scientific Research. issuing body, and Stanford University. Department of Mechanical Engineering. sponsor (page images at HathiTrust)
• Continued computational investigation of MEMS : hybrid surfaces /, by David B. Goldstein, University of Texas at Austin. Department of Aerospace Engineering and Engineering Mechanics. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Direct numerical simulation of compressible turbulent flows using adaptive spectral element method /, by T. J. Chung, K. T. Yoon, University of Alabama in Huntsville. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Turbulence structure associated with intercomponent and interscale energy transfer, and modification by forcing /, by James G. Brasseur, Pennsylvania State University. Department of Mechanical Engineering. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Numerical investigation of surface curvature effects in compressible turbulent flows /, by Linda D. Kral, John F. Donovan, McDonnell Douglas Aerospace (Firm). sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• The Structure of high Reynolds Number turbulent boundary layers /, by Alexander J. Smits, Princeton University. Department of Mechanical and Aerospace Engineering. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Development and validation of RNG methodology for compressible turbulence /, by George Karniadakis, United States. Air Force. Office of Scientific Research. issuing body, and Rutgers University. Department of Mechanical & Aerospace Engineering. sponsor (page images at HathiTrust)
• The Structure of high Reynolds Number turbulent boundary layers : Part A /, by James G. Brasseur, Pennsylvania State University. Department of Mechanical Engineering. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Turbulent flow control /, by William C. Reynolds, issuing body United States. Air Force. Office of Scientific Research, and sponsor Stanford University. Department of Mechanical Engineering (page images at HathiTrust)
• Study of the pressure rise across shock waves required to separate laminar and turbulent boundary layers / (Washington, D.C. : 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)

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