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Viscous flow

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• Fluid dynamics
• Viscosity

• Navier-Stokes equations
• Non-Newtonian fluids
• Reynolds number
• Unsteady viscous flow

• A streambed-particle model-study facility using hydroxyethylcellulose solutions as a fluid / ([New Orleans] : U.S. Dept. of Agriculture, Agricultural Research Service, Southern Region, 1976), by Neil L. Coleman, Wilbert M. Ellis, and United States. Agricultural Research Service. Southern Region (page images at HathiTrust)
• The effect of high viscosity on the flow around a cylinder and around a sphere / (Washington, D.C. : NACA, 1952), by F. Homann and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Hopf bifurcation in the driven cavity / ([Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, Institute for Computational Mechanics in Propulsion, 1989), by John W. Goodrich, Kadosa Halasi, Karl E. Gustafson, and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)
• Multigrid calculation of three-dimensional viscous cascade flows ([Cleveland, Ohio]: NASA, Institute for Computational Mechanics in Propulsion, Lewis Research Center, ; [Springfield, Va. : Available from the National Technical Information Service], 1991), by Andrea Arnone, Louis A. Povinelli, M. S. Liou, and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)
• An implicit finite-difference solution to the viscous shock layer, including the effects of radiation and strong blowing / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by L. Bernard Garrett, John N. Perkins, G. Louis Smith, and Langley Research Center (page images at HathiTrust)
• Hypersonic viscous shock layer of nonequilibrium dissociating gas / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1961), by Paul M. Chung (page images at HathiTrust)
• A theoretical method for the analysis and design of axisymmetric bodies / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by T. D. Beatty, Langley Research Center, and McDonnell Douglas Corporation (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)
• An upwind-biased, point-implicit relaxation algorithm for viscous, compressible perfect-gas flows / (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 Peter A. Gnoffo and Langley Research Center (page images at HathiTrust)
• A viscous/potential flow interaction analysis method for multi-element infinite swept wings. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by F. A. Dvorak, F. A. Woodward, and inc Flow Research (page images at HathiTrust)
• Numerical solution of the hypersonic viscous-shock-layer equations for laminar, transitional, and turbulent flows of a perfect gas over blunt axially symmetric bodies / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by E. Clay Anderson, James N. Moss, and Langley Research Center (page images at HathiTrust)
• Transport properties of N₂ gas at cryogenic temperatures / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Walter E. Pearson and Ames Research Center (page images at HathiTrust)
• Aeroacoustic and aerodynamic applications of the theory of nonequilibrium thermodynamics / (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 W. Clifton Horne, Krishnamurty Karamcheti, Charles A. Smith, and Ames Research Center (page images at HathiTrust)
• An upwind-biased space marching algorithm for supersonic viscous flow / (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, 1991), by Francis A. Greene and Langley Research Center (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)
• Propagation of waves of finite amplitude in thermoviscous media / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1966), by Ervin Y. Rodin, Wyle Laboratories, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• SL4 code : a user's manual / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Y. S. Chou, Ames Research Center, and Lockheed Missiles and Space Company (page images at HathiTrust)
• Radiative coupled viscous flow with massive blowing / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1973), by Y. S. Chou, Ames Research Center, and Lockheed Missiles and Space Company (page images at HathiTrust)
• The VISC code : a user's manual / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Ken Wilson, Ames Research Center, and Lockheed Missiles and Space Company (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)
• An analysis method for two-dimensional transonic viscous flow / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Paul C. Bavitz and Langley Research Center (page images at HathiTrust)
• Numerical calculation of transonic boattail flow / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Wen L. Chow, Bernhard H. Anderson, Lawrence J. Bober, and Lewis Research Center (page images at HathiTrust)
• Transient viscous flow around an elliptic cylinder / (Urbana, Illinois : Dept. of Computer Science, University of Illinois at Urbana-Champaign, 1974), by Gary Arthur Roediger (page images at HathiTrust)
• Least-squares solution of incompressible Navier-Stokes equations with the P-version of finite elements ([Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1991]), by Bo-nan Jiang, Vijay Sonnad, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lattice gas dynamics. (Hanscom Air Force Base, MA : Phillips Laboratory, Directorate of Geophysics, Air Force Materiel Command, 1995), by Jeffrey Yepez and USAF Phillips Laboratory. Directorate of Geophysics (page images at HathiTrust)
• Low Reynolds number two-equation modeling of turbulent flows ([Washington, D.C.] : NASA ; [Springfield, Va. : For sale by the National Technical Information Service, 1991]), by V. Michelassi, T.-H. Shih, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Added masses and forces on two bodies approaching central impact in an inviscid fluid / (Iowa City, Iowa : Iowa Institute of Hydraulic Research, University of Iowa, 1991), by Louis Landweber, Ali Shahshahan, and Iowa Institute of Hydraulic Research (page images at HathiTrust; US access only)
• An extension to lower pressures of the Navier-Stokes theory for the viscous flow of gases between relatively rotating coaxial cylinders / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Willard E. Meador, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Investigation of isothermal, compressible flow across a rotating sealing dam. (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by John Zuk, Lawrence P. Ludwig, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Investigation of isothermal, compressible flow across a rotating sealing dam. (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by John Zuk, Lawrence P. Ludwig, Patricia J. Smith, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• An implicit numerical scheme for the simulation of internal viscous flows on unstructured grids / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994), by Philip C. E. Jorgenson, Richard H. Pletcher, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A new k-[epsilon] eddy viscosity model for high Reynolds number turbulent flows : model development and validation / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• A note on the wave action density of a viscous instability mode on a laminar free-shear flow / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994), by Thomas F. Balsa and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by James T. Howlett, Samuel R. Bland, and Langley Research Center (page images at HathiTrust)
• Viscous-inviscid calculations of jet entrainment effects on the subsonic flow over nozzle afterbodies / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Richard G. Wilmoth, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• The disturbance flow field produced by an evolving vortex / (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 T. B. Gatski and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (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)
• Calculation of unsteady transonic flows with mild separation by viscous-inviscid interaction / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by James T. Howlett and Langley Research Center (page images at HathiTrust)
• Updated users' guide for TAWFIVE with multigrid / (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 N. Duane Melson and Craig L. Streett (page images at HathiTrust)
• Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage / (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 Ronald J. Steinke and Lewis Research Center (page images at HathiTrust)
• Numerical analysis of the scramjet-inlet flow field by using two-dimensional Navier-Stokes equations / (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 Ajay Kumar, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Numerical calculations of viscous compressible fluid flow around a stationary cylinder / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by John G. Trulio, Leonard Walitt, George C. Marshall Space Flight Center, and inc Applied Theory (page images at HathiTrust)
• Numerical calculation of viscous compressible fluid flow around an oscillating rigid cylinder / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by John G. Trulio, Leonard Walitt, George C. Marshall Space Flight Center, and inc Applied Theory (page images at HathiTrust)
• Analytical comparison of hypersonic flight and wind tunnel viscous/inviscid flow fields / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by H. J. Fivel, L. J. Mockapetris, R. V. Masek, Langley Research Center, and McDonnell Douglas Astronautics Company-East (page images at HathiTrust)
• Hypersonic ionizing air viscous shock-layer flows over nonanalytic blunt bodies / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by Miner. E. W. (Earnest Wade), Clark H. Lewis, Lyndon B. Johnson Space Center, and Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Dept (page images at HathiTrust)
• A unified viscous theory of lift and drag of 2-D thin airfoils and 3-D thin wings / (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 John E. Yates and Titan Corporation. California Research & Technology Division. A.R.A.P. Group (page images at HathiTrust)
• Viscous computations of cold air/air flow around scramjet nozzle afterbody / (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 Oktay Baysal, Walter C. Englelund, Old Dominion University. Dept. of Mechanical Engineering and Mechanics, and Langley Research Center (page images at HathiTrust)
• An implicit method for the calculation of inlet flow fields / (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 Sedat Biringen, Oden J. McMillan, Nielsen Engineering & Research, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Reacting viscous-shock-layer solutions with multicomponent diffusion and mass injection / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by James N. Moss and Langley Research Center (page images at HathiTrust)
• Mass flux similarity for slotted transonic-wind-tunnel walls / (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 Joel L. Everhart, Suresh H. Goradia, and Langley Research Center (page images at HathiTrust)
• A hybridized method for computing high-reynolds-number hypersonic flow about blunt bodies / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by K. James Weilmuenster, H. Harris Hamilton, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Mathematical model for two-dimensional multi-component airfoils in viscous flow / (Washington, D.C. : National Aeronautics and Space Administration, 1971), by W. A. Stevens, J. A. Braden, Suresh H. Goradia, and Lockheed-Georgia Company (page images at HathiTrust)
• Investigation of nonlinear inviscid and viscous flow effects in the analysis of dynamic stall / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Peter Crimi, Langley Research Center, and Avco Corporation. Systems Division (page images at HathiTrust)
• Computer user's guide for a chemically reacting viscous shock-layer program / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by E. W. Miner, Clark H. Lewis, Lyndon B. Johnson Space Center, and Virginia Polytechnic Institute and State University. Aerospace and Ocean Engineering Dept (page images at HathiTrust)
• Higher-order numerical methods derived from three-point polynomial interpolation / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1976]), by Stanley G. Rubin, Prem K. Khosla, Langley Research Center, and Nassau County General Applied Science Laboratories (Westbury (page images at HathiTrust)
• Numerical computation of transonic flows by finite-element and finite-diffence methods / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. for sale by the National Technical Information Service, 1978), by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, M. M. Hafez, Langley Research Center, and inc Flow Research (page images at HathiTrust)
• Viscous theory of surface noise interaction phenomena / (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 John E. Yates, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Development of a locally mass flux conservative computer code for calculating 3-D viscous flow in turbomachines / (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 Leonard Walitt, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Simulation of two-dimensional viscous flow through cascades using a semi-elliptic analysis and hybrid C-H grids / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1988), by R. Ramamurti, K. N. Ghia, U. Ghia, and Lewis Research Center (page images at HathiTrust)
• Hypersonic viscous drag on cones in rarefied flow / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by M. I. Kussoy, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental and theoretical low-speed aerodynamic characterisitics of a Wortmann airfoil as manufactured on a fiberglass sailplane / (Washington : National Aeronautics and Space Administration : Springfield, Va. : For sale by the National Technical Information Service, 1977), by Dan M. Somers and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of real-gas and viscous effects on the aerodynamic characteristics of a 40 ̊half-cone with suggested correlations for the shuttle orbiter / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by James L. Hunt, William C. Woods, Robert A Jones, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Computer program for viscous, isothermal compressible flow across a sealing dam with small tilt angle / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by John Zuk, Patricia Jean Smith, and Lewis Research Center (page images at HathiTrust)
• Viscous flow in a short cylindrical vortex chamber with a finite swirl ratio / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Robert W. Hornbeck, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Location of separation on a circular cylinder in crossflow as a function of Reynolds Number / (Bethesda, Md. : Naval Ship Research and Development Center, [1971]), by David W. Coder and Naval Ship Research and Development Center (page images at HathiTrust)
• Governing equations for viscous compressible flow / (Bethesda, Md. : David W. Taylor Naval Ship Research and Development Center, 1978), by William J. H. Smithey and David W. Taylor Naval Ship Research and Development Center (page images at HathiTrust)
• Investigation of viscous flow in glass during phase separation / ([Washington] : National Bureau of Standards, 1973), by Joseph H. Simmons (page images at HathiTrust)
• Viscous effect on surface waves generated by steady disturbances / (Pasadena : California Institute of Technology, Engineering Division, 1958), by Theodore Y.-T. Wu, R. E. Messick, United States. Office of Naval Research, and Pasadena California Institute of Technology. Engineering Division (page images at HathiTrust; US access only)
• A method for computing nonsteady, incompressible, viscous fluid flows / (Los Alamos, N.M. : Los Alamos Scientific Laboratory of the University of California, 1963), by Jacob E. Fromm, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (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)
• The molecular and viscous effusion of saturated vapors / (Argonne, Ill. : Argonne National Laboratory, 1960), by K. Douglas Carlson, U.S. Atomic Energy Commission. ANL., and Argonne National Laboratory. ANL. (page images at HathiTrust)
• Pressure distribution and some effects of viscosity on slender inclined bodies of revolution / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by H. Julian Allen and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Effect of variable viscosity and thermal conductivity on high-speed slip flow between concentric cylinders / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by T. C. Lin, R. E. Street, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Viscous shock-layer flow in the windward plane of cones at angle of attack /, by R. R Eaton, P. C. Kaestner, Sandia Corporation, and U.S. Atomic Energy Commission (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)
• Computations of the nonequilibrium flow of a viscous, radiating fluid about a blunt axisymmetric body., by J. T. Curtis, C. R. Strom, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Cornell Aeronautical Laboratory (page images at HathiTrust)
• Computations of the nonequilibrium flow of a viscous, radiating fluid about a blunt axisymmetric body., by J. T. Curtis, C. R. Strom, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Cornell Aeronautical Laboratory (page images at HathiTrust)
• The SMAC method : a numerical technique for calculating incompressible fluid flows /, by A. A. Amsden, Francis H. Harlow, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (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)
• Efficient ADI and spline ADI methods for the Navier-Stokes equations /, by Michele Napolitano, sponsor Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor University of Dayton. Research Institute (page images at HathiTrust)
• The blunt body viscous layer problem with and without an applied magnetic field /, by Hakurō Oguchi, United States. Air Force. Air Research and Development Command. issuing agency, United States. Wright Air Development Center. sponsor, and sponsor Brown University. Division of Engineering (page images at HathiTrust)
• Computation of three-dimensional supersonic viscous flows in internal corners /, by John C. Tannehill, Dale A. Anderson, issuing agency Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and Inc. Engineering Analysis (page images at HathiTrust)
• A Study of laminar heat transfer to spherically blunted cones and hemisphere-cylinders at hypersonic conditions /, by B. J. Griffith, Clark H. Lewis, Inc. AEDC Division. sponsor Sverdrup/ARO, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• PARC code : theory and usage /, by G. K. Cooper, J. R. Sirbaugh, Inc. sponsor Sverdrup Technology, United States. Air Force. Arnold Air Force Base. sponsor, and Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• Second moment closure modeling of complex turbulent flows /, by Sharath Girimaji, Lawrence Ukeiley, Mark N. Glauser, Jeremy T. Pinier, sponsor Texas A & M University. Aerospace Engineering Department, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• The Sharp leading edge problem in hypersonic flow /, by Hakuro Oguchi, United States. Air Force. Aeronautical Research Laboratories. issuing body, and Brown University. Division of Engineering. sponsor (page images at HathiTrust)
• An efficient hybrid grid scheme for calculation of viscous flows /, by Ralph W. Noack, David G. Bishop, and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Solution-adaptive calculation of unsteady blade row interactions in transonic turbomachinery /, by Scott M. Richardson and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• 3-D composite velocity solutions for subsonic/transonic flow over forebodies and afterbodies /, by Raymond E. Gordnier, Inc. Universal Energy Systems, sponsor Wright Research and Development Center, sponsor Air Force Flight Dynamics Laboratory (U.S.), and issuing body United States. Air Force. Systems Command (page images at HathiTrust)
• Computation of viscous shock/shock hypersonic interactions with an implicit flux split scheme /, by Datta Gaitonde, Inc. Universal Energy Systems, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, sponsor Air Force Flight Dynamics Laboratory (U.S.), and issuing body United States. Air Force. Systems Command (page images at HathiTrust)
• An upwind method for the solution of the 3D Euler and Navier-Stokes equations on adaptively meshes /, by Michael J. Aftosmis and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• High-speed viscous flows past blunt bodies and compression corners with flux-split methods /, by Datta V. Gaitonde and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• A study of flow separation in regions of shock wave-boundary layer interaction in hypersonic flow /, by Michael S. Holden, issuing body Aerospace Research Laboratories (U.S.), and sponsor New York University. Aerospace and Energetics Laboratory (page images at HathiTrust)
• Development and application of new algorithms for the simulation of viscous compressible flows with moving bodies in three dimensions /, by Rainald Lohner, Juan R. Cebral, Chi Yang, issuing body United States. Air Force. Office of Scientific Research, and sponsor George Mason University (page images at HathiTrust)
• An analysis of transonic viscous/inviscid interactions on axisymmetric bodies with solid strings or real plumes /, by Steven F. Yaros, Inc. sponsor ARO, United States. Air Force. Arnold Air Force Base. sponsor, and United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body (page images at HathiTrust)
• Preliminary experimental results of the reduction of viscous effects in a low-density supersonic nozle by wall cryopumping /, by W. N. MacDermott, Arnold Engineering Development Center. issuing body, Inc. sponsor ARO, and United States. Air Force. Air Research and Development Command. sponsor (page images at HathiTrust)
• Energy-based design methodology for air vehicle systems : aerodynamic correlation study /, by Richard S. Figliola, Clemson University. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Low-density flow effects for hypervelocity vehicles : phase II /, by Roop N. Gupta, Sudheer N. Nayani, Inc. ViGYAN, sponsor Wright Research and Development Center, sponsor Air Force Flight Dynamics Laboratory (U.S.), and issuing body United States. Air Force. Systems Command (page images at HathiTrust)
• On three-dimensional free-mixing /, by Martin H Bloom, issuing body United States. Air Force. Office of Scientific Research, and sponsor Polytechnic Institute of Brooklyn. Department of Aeronautical Engineering and Applied Mechanics (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)
• Separated flow studies /, by Wilbur L. Hankey and issuing body Aerospace Research Laboratories (U.S.) (page images at HathiTrust)
• Hypersonic viscous flow /, by Hsien K. Cheng, University of Southern California. Department of Aerospace Engineering. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
• Behavior of solutions of the Navier-Stokes equations for a complete class of three-dimensional viscous vortices /, by Coleman duP. Donaldson, Roger D. Sullivan, sponsor Aeronautical Research Associates of Princeton, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)

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