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Viscous flow

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• Fluid dynamics
• Viscosity

• Viscous flow -- Computer programs
• Viscous flow -- Computer simulation
• Viscous flow -- Congresses
• Viscous flow -- Data processing
• Viscous flow -- Mathematical models
• Viscous flow -- Mathematics
• Viscous flow -- Measurement
• Viscous flow -- Mixing
• Navier-Stokes equations
• Non-Newtonian fluids
• Reynolds number
• Unsteady viscous flow

• The molecular and viscous effusion of saturated vapors (Argonne National Laboratory, 1960), by K. Douglas Carlson (page images at HathiTrust)
• Investigation of viscous flow in glass during phase separation (National Bureau of Standards, 1973), by Joseph H. Simmons (page images at HathiTrust)
• Viscous fluids (Phillips Laboratory, Directorate of Geophysics, Air Force Materiel Command, 1995), by Jeffrey Yepez and USAF Phillips Laboratory. Directorate of Geophysics (page images at HathiTrust)
• Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by James T. Howlett, Samuel R. Bland, and Langley Research Center (page images at HathiTrust)
• An implicit numerical scheme for the simulation of internal viscous flows on unstructured grids (National Aeronautics and Space Administration ;, 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 (National Aeronautics and Space Administration ;, 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 (National Aeronautics and Space Administration ;, 1994), by Thomas F. Balsa and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aeroacoustic and aerodynamic applications of the theory of nonequilibrium thermodynamics (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by W. Clifton Horne, Krishnamurty Karamcheti, Charles A. Smith, and Ames Research Center (page images at HathiTrust)
• Mass flux similarity for slotted transonic-wind-tunnel walls (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by Joel L. Everhart, Suresh H. Goradia, and Langley 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 (National Aeronautics and Space Administration ;, 1974), by Josef Rom, Lawrence J. Bober, and Lewis Research Center (page images at HathiTrust)
• Low Reynolds number two equation modeling of turbulent flows (NASA ;, 1991), by V. Michelassi, T.-H. Shih, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Least-squares solution of incompressible Navier-Stokes equations with the P-version of finite elements (National Aeronautics and Space Administration ;, 1991), by Bo-nan Jiang, Vijay Sonnad, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Hopf bifurcation in the driven cavity (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 (NASA, Institute for Computational Mechanics in Propulsion, Lewis Research Center, ;, 1991), by Andrea Arnone, Louis A. Povinelli, M. S. Liou, and Lewis Research Center. Institute for Computational Mechanics in Propulsion (page images at HathiTrust)
• Numerical calculations of viscous compressible fluid flow around a stationary cylinder (National Aeronautics and Space Administration ;, 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 (National Aeronautics and Space Administration ;, 1969), by John G. Trulio, Leonard Walitt, George C. Marshall Space Flight Center, and inc Applied Theory (page images at HathiTrust)
• Propagation of waves of finite amplitude in thermoviscous media (National Aeronautics and Space Administration ;, 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)
• Spiral longitudinal vortices ... (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)
• Investigation of nonlinear inviscid and viscous flow effects in the analysis of dynamic stall (National Aeronautics and Space Administration ;, 1974), by Peter Crimi, Langley Research Center, and Avco Corporation. Systems Division (page images at HathiTrust)
• Analytical comparison of hypersonic flight and wind tunnel viscous/inviscid flow fields (National Aeronautics and Space Administration ;, 1975), by H. J. Fivel, L. J. Mockapetris, R. V. Masek, Langley Research Center, and McDonnell Douglas Astronautics Company-East (page images at HathiTrust)
• A viscous/potential flow interaction analysis method for multi-element infinite swept wings. Volume I (National Aeronautics and Space Administration ;, 1974), by F. A. Dvorak, F. A. Woodward, and inc Flow Research (page images at HathiTrust)
• A theoretical method for the analysis and design of axisymmetric bodies (National Aeronautics and Space Administration ;, 1975), by T. D. Beatty, Langley Research Center, and McDonnell Douglas Corporation (page images at HathiTrust)
• Viscous theory of surface noise interaction phenomena (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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)
• Radiative coupled viscous flow with massive blowing (National Aeronautics and Space Administration ;, 1973), by Y. S. Chou, Ames Research Center, and Lockheed Missiles and Space Company (page images at HathiTrust)
• An implicit method for the calculation of inlet flow fields (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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)
• Hypersonic viscous shock layer of nonequilibrium dissociating gas (National Aeronautics and Space Administration ;, 1961), by Paul M. Chung (page images at HathiTrust)
• NASA TN D-4036 (National Aeronautics and Space Administration ;, 1967), by M. I. Kussoy, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6092 (National Aeronautics and Space Administration :, 1970), by Willard E. Meador, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Experimental and theoretical low-speed aerodynamic characterisitics of a Wortmann airfoil as manufactured on a fiberglass sailplane (National Aeronautics and Space Administration :, 1977), by Dan M. Somers and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Numerical calculation of transonic boattail flow (National Aeronautics and Space Administration ;, 1975), by Wen L. Chow, Bernhard H. Anderson, Lawrence J. Bober, and Lewis Research Center (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 (National Aeronautics and Space Administration ;, 1977), by James L. Hunt, William C. Woods, Robert A Jones, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5344 (National Aeronautics and Space Administration ;, 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)
• NASA TN D-5345 (National Aeronautics and Space Administration ;, 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 finite-difference solution to the viscous shock layer, including the effects of radiation and strong blowing (National Aeronautics and Space Administration ;, 1972), by L. Bernard Garrett, John N. Perkins, G. Louis Smith, and Langley Research Center (page images at HathiTrust)
• Transport properties of N₂ gas at cryogenic temperatures (National Aeronautics and Space Administration ;, 1974), by Walter E. Pearson and Ames Research Center (page images at HathiTrust)
• Relaxation of an unsteady turbulent boundary layer on a flat plate in an expansion tube (National Aeronautics and Space Administration ;, 1974), by Roop N. Gupta, Robert L. Trimpi, and Langley Research Center (page images at HathiTrust)
• Location of separation on a circular cylinder in crossflow as a function of Reynolds Number (Naval Ship Research and Development Center, 1971), by David W. Coder and Naval Ship Research and Development Center (page images at HathiTrust)
• The effect of high viscosity on the flow around a cylinder and around a sphere (NACA, 1952), by F. Homann and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• Pressure distribution and some effects of viscosity on slender inclined bodies of revolution (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 (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)
• Transient viscous flow around an elliptic cylinder (Dept. of Computer Science, University of Illinois at Urbana-Champaign, 1974), by Gary Arthur Roediger (page images at HathiTrust)
• Viscous effect on surface waves generated by steady disturbances (California Institute of Technology, Engineering Division, 1958), by Theodore Y.-T. Wu, R. E. Messick, United States. Office of Naval Research, and California Institute of Technology. Engineering Division (page images at HathiTrust; US access only)
• A streambed-particle model-study facility using hydroxyethylcellulose solutions as a fluid (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)
• Analytical procedures used to obtain and evaluate the eddy viscosity and mixing length extracted from incompressible turbulent boundary layer data (Silver Spring, Maryland : Naval Ordnance Laboratory, 1974., 1974), by W. J. Glowacki and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Computations of the nonequilibrium flow of a viscous, radiating fluid about a blunt axisymmetric body. Volume I, Equations and Results (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), by J. T. Curtis, C. R. Strom, Air Force Flight Dynamics Laboratory (U.S.), and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Computations of the nonequilibrium flow of a viscous, radiating fluid about a blunt axisymmetric body. Volume II, Program details and operating procedure (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1967., 1967), by J. T. Curtis, C. R. Strom, Air Force Flight Dynamics Laboratory (U.S.), and Cornell Aeronautical Laboratory (page images at HathiTrust)
• Efficient ADI and spline ADI methods for the Navier-Stokes equations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), by Michele Napolitano, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and University of Dayton. Research Institute (page images at HathiTrust)
• Computation of three-dimensional supersonic viscous flows in internal corners (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1980., 1980), by John C. Tannehill, Dale A. Anderson, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Inc Engineering Analysis (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 (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984., 1984), by Md.) U.S. Air Force/Federal Republic of Germany Data Exchange Agreement Meeting (9th : 1984 : Silver Springs, Anthony W. Fiore, Air Force Flight Dynamics Laboratory (U.S.), and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• The blunt body viscous layer problem with and without an applied magnetic field (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, United States Air Force, 1960., 1960), by Hakurō Oguchi, United States. Air Force. Air Research and Development Command, United States. Wright Air Development Center, and Brown University. Division of Engineering (page images at HathiTrust)
• A Study of laminar heat transfer to spherically blunted cones and hemisphere-cylinders at hypersonic conditions (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1963., 1963), by B. J. Griffith, Clark H. Lewis, Inc. AEDC Division Sverdrup/ARO, and Arnold Engineering Development Center (page images at HathiTrust)
• Preliminary experimental results of the reduction of viscous effects in a low-density supersonic nozle by wall cryopumping (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Research and Development Command, United States Air Force, 1961., 1961), by W. N. MacDermott, Arnold Engineering Development Center, Inc ARO, and United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• A study of flow separation in regions of shock wave-boundary layer interaction in hypersonic flow (Wright-Patterson Air Force Base, Ohio : Aerospace Research Laboratories, Air Force Systems Command, 1975., 1975), by Michael S. Holden, Aerospace Research Laboratories (U.S.), and New York University. Aerospace and Energetics Laboratory (page images at HathiTrust)
• PARC code : theory and usage (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), by G. K. Cooper, J. R. Sirbaugh, Inc Sverdrup Technology, United States. Air Force. Arnold Air Force Base, and Arnold Engineering Development Center (page images at HathiTrust)
• Second moment closure modeling of complex turbulent flows (Arlington, Virginia. : Air Force Office of Scientific Research, 2007., 2007), by Sharath Girimaji, Lawrence Ukeiley, Mark N. Glauser, Jeremy T. Pinier, Texas A & M University. Aerospace Engineering Department, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Solution-adaptive calculation of unsteady blade row interactions in transonic turbomachinery (Wright-Patterson Air Force Base, Ohio : Aero Propulsion and Power Directorate, Wright Laboratory, Air Force Materiel Command, United States Air Force, 1996., 1996), by Scott M. Richardson and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Development and application of new algorithms for the simulation of viscous compressible flows with moving bodies in three dimensions (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, United States Air Force, 1996., 1996), by Rainald Löhner, Juan R. Cebral, Chi Yang, United States. Air Force. Office of Scientific Research, and George Mason University (page images at HathiTrust)
• Energy-based design methodology for air vehicle systems : aerodynamic correlation study (Arlington, Virginia : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 2005., 2005), by R. S. Figliola, Clemson University, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• An analysis of transonic viscous/inviscid interactions on axisymmetric bodies with solid strings or real plumes (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Propulsion Wind Tunnel Facility, Air Force Systems Command, United States Air Force, 1978., 1978), by Steven F. Yaros, Inc ARO, United States. Air Force. Arnold Air Force Base, and Arnold Engineering Development Center (page images at HathiTrust)
• Viscous flow interaction studies : final report on work unit 7064 02 06 (Wright-Patterson Air Force Base, Ohio : Aerospace Research Laboratories, Air Force Systems Command, 1975., 1975), by Robert H. Korkegi and Aerospace Research Laboratories (U.S.) (page images at HathiTrust)
• 3-D composite velocity solutions for subsonic/transonic flow over forebodies and afterbodies (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research Development Center, Air Force Systems Command, United States Air Force, 1989., 1989), by Raymond E. Gordnier, Inc Universal Energy Systems, Wright Research and Development Center, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Separated flow studies (Wright-Patterson Air Force Base, Ohio : Aerospace Research Laboratories, Air Force Systems Command, 1975., 1975), by Wilbur L. Hankey and Aerospace Research Laboratories (U.S.) (page images at HathiTrust)
• Hypersonic viscous flow (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 1990., 1990), by Hsien K. Cheng, University of Southern California. Department of Aerospace Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Computation of viscous shock/shock hypersonic interactions with an implicit flux split scheme (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Laboratory, Air Force Systems Command, United States Air Force, 1990., 1990), by Datta V. Gaitonde, Inc Universal Energy Systems, Ohio) Wright Laboratory (Wright-Patterson Air Force Base, Air Force Flight Dynamics Laboratory (U.S.), and 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 (Wright-Patterson Air Force Base, Ohio : Fliight Dynamics Directorate, Wright Laboratory, Air Force Materiel Command, 1992., 1992), 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 (Wright-Patterson Air Force Base, Ohio : Fliight Dynamics Directorate, Wright Laboratory, Air Force Systems Command, 1992., 1992), by Datta V. Gaitonde and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Low-density flow effects for hypervelocity vehicles : phase II (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Wright Research Development Center, United States Air Force Systems Command, 1990., 1990), by Roop N. Gupta, Sudheer N. Nayani, Inc ViGYAN, Wright Research and Development Center, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• An assessment of viscous effects in computational simulation of benign and burst vortex flows on generic fighter wind-tunnel models using TEAM code (National Aeronautics and Space Administration, Langley Research Center ;, 1995), by Tim A. Kinard, Pradeep Raj, Brenda W. Harris, and Langley Research Center (page images at HathiTrust)
• Design optimization of natural laminar flow bodies in compressible flow (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993), by Simha S. Dodbele, Langley Research Center, and Inc ViGYAN (page images at HathiTrust)
• Generation of the starting plane flowfield for supersonic flow over a spherically capped body (Silver Spring, Maryland : Naval Surface Weapons Center, Research and Technology Department, 1985., 1985), by Tsuying Hsieh, F. J. Priolo, and Naval Surface Weapons Center (page images at HathiTrust)

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