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Flow visualization

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• Fluid dynamics

• Particle image velocimetry

• Visualization of flow

• Flow-separation patterns on symmetric forebodies / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1986), by Earl R. Keener (page images at HathiTrust)
• Visual study of swirling and nonswirling two-phase two-component flow at 1 and 0 gravity / (Washington, D.C. : National Aeronautics and Space Administration, [1963]), by David G. Evans and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation in an annular cascade sector of highly loaded turbine stator blading. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by James L. Bettner, Lewis Research Center, and General Motors Corporation (page images at HathiTrust)
• Laser Doppler velocity measurements of swirling flows with upstream influence / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1973), by Kenneth L. Orloff, Hartmut H. Bossel, and Santa Barbara University of California (page images at HathiTrust)
• A simplified molecular model for studying vibration-dissociation coupling in fluid flows / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969), by Walter Albert Reinhardt, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Detailed flow-field measurements over a 75 ̊swept delta wing / (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 Scott O. Kjelgaard, William L. Sellers, and Langley Research Center (page images at HathiTrust)
• Finite element analysis and computer graphics visualization of flow around pitching and plunging airfoils / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Theodore Bratanow, Akin Ecer, Langley Research Center, and University of Wisconsin--Milwaukee (page images at HathiTrust)
• Aerodynamic and flow-visualization studies of variations in the geometry of irregular planform wings at a Mach number of 20.3 / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by David R. Stone, Bernard Spencer, and Langley Research Center (page images at HathiTrust)
• Vortex shedding from a blunt trailing edge with equal and unequal external mean velocities / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Paul F. Brinich, Marvin E. Goldstein, Donald R. Boldman, and Lewis Research Center (page images at HathiTrust)
• Numerical solution of the unsteady Navier-Stokes equations and application to flow in a rectangular cavity with a moving wall / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Leo F. Donovan, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Measurements of boundary layer transition, separation and streamline direction on rotating blades / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by William J. McCroskey, U.S. Army Air Mobility Research and Development Laboratory, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• A Pulse-forming network for particle path visualization / (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 Kenneth W. McAlister, Army Research and Technology Laboratories (U.S.), United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Aeromechanics Laboratory (page images at HathiTrust)
• Flow visualization study of the horseshoe vortex in a turbine stator cascade / (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 Raymond E. Gaugler, Louis M. Russell, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Pockels-effect cell for gas-flow simulation / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : National Technical Information Service], 1982), by David Weimer, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
• Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988), by John E. Lamar, Thomas D. Johnson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Digital enhancement of flow field images / (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 Robert A. Kudlinski, Stephen Keith Park, and Langley Research Center (page images at HathiTrust)
• Streamlines in a steady flow / ([Washington, D.C. : ] National Aeronautics and Space Administration, [1966]), by Robert Legendre (page images at HathiTrust)
• Investigation of flow characteristics over missle bodies at supersonic speeds / (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 Raymond L. Barger, Wallace C. Sawyer, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Visualization techniques to experimentally model flow and heat transfer in turbine and aircraft flow passages / (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 Louis M. Russell and Steven A. Hippensteele (page images at HathiTrust)
• Evaluation of diffuse-illumination holographic cinematography in a flutter cascade / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Arthur J. Decker and Lewis Research Center (page images at HathiTrust)
• New technique for experimental generation of two-dimensional blade-vortex interaction at low Reynolds numbers / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986), by Earl R. Booth, James C. Yu, and Langley Research Center (page images at HathiTrust)
• Combined single-pulse holography and time-resolved laser schlieren for flow visualization / (Washington, D.C. : U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Alpheus W. Burner, William K. Goad, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Holographic flow visualization at the Langley Expansion Tube / (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 William K. Goad, Alpheus W. Burner, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Flow visualization and interpretation of visualization data for deflected thrust V/STOL nozzles ([Washington, D.C. : National Aeronautics and Space Administration, 1984]), by H. C. Kao, Albert L. Johns, Paul L. Burstadt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Operational performance of vapor-screen systems for in-flight visualization of leading-edge vortices on the F-106B aircraft / (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 John E. Lamar (page images at HathiTrust)
• A smoke generator system for aerodynamic flight research / (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 David M. Richwine, Gene V. Tracy, Robert E. Curry, and Dryden Flight Research Facility (page images at HathiTrust)
• Flow visualization studies of blowing from the tip of a swept wing / (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 Jeannette W. Smith, Dan H. Neuhart, Raymond E. Mineck, and Langley Research Center (page images at HathiTrust)
• In-flight flow visualization characteristics of the NASA F-18 high alpha research vehicle at high angles of attack / (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 David F. Fisher, David M. Richwine, John H. Del Frate, and Dryden Flight Research Facility (page images at HathiTrust)
• Flow visualization of film cooling with spanwise injection from a small array of holes and compound-angle injection from a large array / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : for sale by the National Technical Information Service, 1978.), by Louis M. Russell and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Some flow phenomena associated with aligned, sequential apertures with borda-type inlets / (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 Robert C. Hendricks, T. Trent Stetz, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (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)
• A Synchronous strobed laser light sheet for rotor flow visualization / (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 Bradley D. Leighty and Langley Research Center (page images at HathiTrust)
• Wind tunnel investigation of simulated helicopter engine exhaust interacting with windstream / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974), by Craig S. Shaw, John C. Wilson, and Langley Research Center (page images at HathiTrust)
• Holography through optically active windows / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by Arthur J. Decker, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Streakline flow visualization of discrete-hole film cooling with normal, slanted and compound angle injection / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Raymond S. Colladay, Louis M. Russell, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Computer solution of unsteady Navier-Stokes equations for an infinite hydrodynamic step bearing / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and technical Information, Springfield, Va. 22151], 1970), by Henry A. Putre, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Wind-tunnel calibration of a 40° conical pressure probe at Mach numbers from 3.5 to 7.4 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Frank W. Burcham, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Preliminary investigation of the use of afterglow for visualizing low-density compressible flows / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Thomas W. Williams, James M. Benson, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• The use of a luminescent lacquer for the visual indication of boundary-layer transition / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Jackson R. Stalder, Ellis G. Slack, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• A visualization study of secondary flows in cascades / (Washington, D.C. : National Advisory Committee for Aeronautics, [1953]), by Arthur G. Hansen, George R. Costello, Howard Z. Herzig, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Comparison of secondary flows and boundary-layer accumulations in several turbine nozzles / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by Milton G. Kofskey, Howard Z. Herzig, Hubert W. Allen, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Separated flow phenomena on a slender cone at Mach 5 /, by Robert H. Feldhuhn, Allen E. Winkelmann, 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)
• Flow visualization workshop report /, by William C. Ragsdale, Md.) Naval Ordnance Laboratory (White Oak, United States. Naval Air Systems Command, and Md.) Workshop on Flow Visualization and Flow Measurement Techniques (1971 : Silver Spring (page images at HathiTrust)
• The physical properties of active nitrogen in low-density flow / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by James M. Benson and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Flow visualization : a comparison of streaming birefringence with other techniques / (Richland, Wash. : Pacific Northwest Laboratory, 1965), by Donald Henry White, General Electric Company, U.S. Atomic Energy Commission, and Pacific Northwest Laboratory (page images at HathiTrust)
• The marriage of optical, tracer and surface indicator techniques in flow visualization /, by Raymond Sedney, Clarence C. Bush, Clarence W. Kitchens, and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• The structure of three-dimensional separated flows in obstacle-boundary layer interactions /, by Raymond Sedney, Clarence W. Kitchens, and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• How to analyze 2-D Schlieren photographs to obtain the density gradient structure of 3-D flow fields /, by Allen E. Winkelmann, Robert H. Feldhuhn, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• An experimental investigation of the flow field around a yawed cone /, by Robert H. Feldhuhn and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• The shock heights of static free jets /, by Richard T. Driftmyer and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Flow field measurements around an ogive-cylinder at angles of attack up to 15 degrees for mach numbers 3.5 and 4 /, by William C. Ragsdale and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Use of phase-change paints to study fin-body interference heating /, by Jr. Gillerlain and Naval Surface Weapons Center. : White Oak Laboratory (page images at HathiTrust)
• Experimental investigation of a fin-cone interference flow field at Mach 5 /, by Jr. Gillerlain and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• an Investigation of the use of holography in studying supersonic flow in inlets. /, by III Spring, W. C. Ragsdale, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• A wind tunnel investigation of jets exhausting into a crossflow., by L. B. Fricke, Henry Ziegler, Peter T. Wooler, sponsor Northrop Corporation. Aircraft Division, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• An investigation of the backflow phenomenon in centrifugal superchargers / (Washington, D.C. : National Advisory Committee for Aeronautics, [1945]), by William A. Benser, Jason J. Moses, Aircraft Engine Research Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Visualization of secondary-flow phenomena in blade row / (Washington, D.C. : National Advisory Committee for Aeronautics, [1952]), by H. Z. Herzig, G. R. Costello, A. G. Hansen, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Pressure and heat transfer measurements for hypersonic flows over expansion corners and ahead of ramps / (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1963-1964), by Louis G. Kaufman, sponsor Air Force Flight Dynamics Laboratory (U.S.), issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Holographic investigation of slender body vortex wakes /, by F. D. Deffenbaugh, J. L. Jacoby, issuing agency Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor TRW Inc. Systems and Energy (page images at HathiTrust)
• Development of an advanced implicit algorithm for MHD computations on parallel supercomputers /, by Uri Shumlak, sponsor University of Washington. College of Engineering, and issuing body United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Two-component simultaneous LDV turbulence measurements in an axisymmetric nozzle afterbody subsonic flow field with a cold, underexpanded supersonic jet /, by F. L. Heltsley, F. L. Crosswy, sponsor Calspan Field Services, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• A flow visualization investigation on selected shapes with emphasis on flow separation /, by M. H Clarkson, United States. Air Force. Systems Command. sponsor, Air Force Armament Laboratory. issuing body, and University of Florida. Department of Engineering Sciences. sponsor (page images at HathiTrust)
• The Influence of high angle of attack flow pheomena on the dynamic stability of slender missiles /, by James M. Jenista, Robert C. Nelson, United States. Air Force. Systems Command. sponsor, Air Force Armament Laboratory. issuing body, and University of Notre Dame. |b Department of Aerospace and Mechanical Engineering. sponsor (page images at HathiTrust)
• Quantitative visualization of turbulent reactive flows in propulsion systems /, by Peyman Givi, Charles T. Brunskill, State University of New York at Buffalo. |b School of Engineering and Applied Sciences. sponsor, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)

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