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Flow visualization

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• Fluid dynamics

• Flow visualization -- Congresses
• Flow visualization -- Equipment and supplies
• Flow visualization -- Mathematical methods
• Flow visualization -- Measurement
• Flow visualization -- Technique
• Particle image velocimetry
• Wind tunnels -- Flow visualization

• Visualization of flow

• Sensitivity of F-106B leading-edge-vortex images to flight and vapor-screen parameters (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 (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1988), by Robert A. Kudlinski, Stephen Keith Park, and Langley Research Center (page images at HathiTrust)
• Investigation of flow characteristics over missle bodies at supersonic speeds (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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)
• A Synchronous strobed laser light sheet for rotor flow visualization (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Bradley D. Leighty and Langley Research Center (page images at HathiTrust)
• Visualization techniques to experimentally model flow and heat transfer in turbine and aircraft flow passages (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by Louis M. Russell and Steven A. Hippensteele (page images at HathiTrust)
• Evaluation of diffuse-illumination holographic cinematography in a flutter cascade (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Earl R. Booth, James C. Yu, and Langley Research Center (page images at HathiTrust)
• A Pulse-forming network for particle path visualization (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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)
• Combined single-pulse holography and time-resolved laser schlieren for flow visualization (U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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 (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)
• Flow-separation patterns on symmetric forebodies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1986), by Earl R. Keener (page images at HathiTrust)
• Operational performance of vapor-screen systems for in-flight visualization of leading-edge vortices on the F-106B aircraft (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1987), by John E. Lamar (page images at HathiTrust)
• Flow visualization studies of blowing from the tip of a swept wing (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Jeannette W. Smith, Dan H. Neuhart, Raymond E. Mineck, and Langley Research Center (page images at HathiTrust)
• Wind tunnel investigation of simulated helicopter engine exhaust interacting with windstream (National Aeronautics and Space Administration ;, 1974), by Craig S. Shaw, John C. Wilson, and Langley Research Center (page images at HathiTrust)
• Holography through optically active windows (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 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)
• Flow visualization study of the horseshoe vortex in a turbine stator cascade (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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)
• Flow visualization of film cooling with spanwise injection from a small array of holes and compound-angle injection from a large array (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 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 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 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)
• Pockels-effect cell for gas-flow simulation (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), by David Weimer, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
• Experimental investigation in an annular cascade sector of highly loaded turbine stator blading. Volume IV, Performance of jet-flapped blade (National Aeronautics and Space Administration ;, 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 (National Aeronautics and Space Administration ;, 1973), by Kenneth L. Orloff, Hartmut H. Bossel, and Santa Barbara University of California (page images at HathiTrust)
• Finite element analysis and computer graphics visualization of flow around pitching and plunging airfoils (National Aeronautics and Space Administration ;, 1973), by Theodore Bratanow, Akin Ecer, Langley Research Center, and University of Wisconsin--Milwaukee (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)
• NASA TR R-324 (National Aeronautics and Space Administration ;, 1969), by Walter Albert Reinhardt, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Vortex shedding from a blunt trailing edge with equal and unequal external mean velocities (National Aeronautics and Space Administration ;, 1975), by Paul F. Brinich, Marvin E. Goldstein, Donald R. Boldman, and Lewis Research Center (page images at HathiTrust)
• Streakline flow visualization of discrete-hole film cooling with normal, slanted and compound angle injection (National Aeronautics and Space Administration ;, 1976), by Raymond S. Colladay, Louis M. Russell, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5682 (National Aeronautics and Space Administration ;, 1970), by Henry A. Putre, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Aerodynamic and flow-visualization studies of variations in the geometry of irregular planform wings at a Mach number of 20.3 (National Aeronautics and Space Administration ;, 1974), by David R. Stone, Bernard Spencer, and Langley Research Center (page images at HathiTrust)
• NASA TN D-1876 (National Aeronautics and Space Administration, 1963), by William Lewis, Robert G. Dorsch, Robert J. Blade, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-1769 (National Aeronautics and Space Administration, 1963), by Charles E. Duller, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-6312 (National Aeronautics and Space Administration ;, 1971), by Leo F. Donovan, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-6321 (National Aeronautics and Space Administration ;, 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)
• Visualization of secondary-flow phenomena in blade row (National Advisory Committee for Aeronautics, 1952), by H. Z. Herzig, G. R. Costello, A. G. Hansen, United States National Advisory Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Preliminary investigation of the use of afterglow for visualizing low-density compressible flows (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 (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)
• The physical properties of active nitrogen in low-density flow (National Advisory Committee for Aeronautics, 1951), by James M. Benson and United States National Advisory Committee for Aeronautics (page images at HathiTrust)
• A visualization study of secondary flows in cascades (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 (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)
• Visual study of swirling and nonswirling two-phase two-component flow at 1 and 0 gravity (National Aeronautics and Space Administration, 1963), by David G. Evans and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Flow visualization : a comparison of streaming birefringence with other techniques (Pacific Northwest Laboratory, 1965), by Donald Henry White, General Electric Company, U.S. Atomic Energy Commission, and Pacific Northwest Laboratory (page images at HathiTrust)
• NACA Wartime Reports. Series E. (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)
• The marriage of optical, tracer and surface indicator techniques in flow visualization (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratories, 1975., 1975), 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 (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratories, 1975., 1975), by Raymond Sedney, Clarence W. Kitchens, and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• Separated flow phenomena on a slender cone at Mach 5 (White Oak, Maryland : United States Naval Ordnance Laboratory, 1969., 1969), by Robert H. Feldhuhn, Allen E. Winkelmann, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• How to analyze 2-D Schlieren photographs to obtain the density gradient structure of 3-D flow fields (White Oak, Maryland : United States Naval Ordnance Laboratory, 1969., 1969), 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 (White Oak, Maryland : United States Naval Ordnance Laboratory, 1969., 1969), by Robert H. Feldhuhn 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 (White Oak, Maryland : United States Naval Ordnance Laboratory, 1970., 1970), by Allen E. Winkelmann and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• The shock heights of static free jets (White Oak, Maryland : United States Naval Ordnance Laboratory, 1972., 1972), 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 (White Oak, Maryland : United States Naval Ordnance Laboratory, 1972., 1972), 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 (Silver Spring, Maryland : Naval Surface Weapons Center, White Oak Laboratory, 1976., 1976), 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 (Silver Spring, Maryland : Naval Surface Weapons Center, 1976., 1976), 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. (Silver Spring, Maryland : Naval Ordnance Laboratory, White Oak, 1973., 1973), by III Spring, W. C. Ragsdale, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
• Pressure and heat transfer measurements for hypersonic flows over expansion corners and ahead of ramps (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1963), by Louis G. Kaufman, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command. Aeronautical Systems Division, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
• Holographic investigation of slender body vortex wakes (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 F. D. Deffenbaugh, J. L. Jacoby, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and TRW Inc. Systems and Energy (page images at HathiTrust)
• A wind tunnel investigation of jets exhausting into a crossflow. Volume 1, Test description and data analysis (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), by L. B. Fricke, Henry Ziegler, Peter T. Wooler, Northrop Corporation. Aircraft Division, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Development of an advanced implicit algorithm for MHD computations on parallel supercomputers (Bolling Air Force Base, D.C. : Air Force Office of Scientific Research, 1998., 1998), by Uri Shumlak, University of Washington. College of Engineering, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Quantitative visualization of turbulent reactive flows in propulsion systems (Arlington, Virginia : Air Force Office of Scientific Research, Air Research and Development Command, United States Air Force, 2002., 2002), by P. Givi, Charles T. Brunskill, State University of New York at Buffalo. |b School of Engineering and Applied Sciences, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• A flow visualization investigation on selected shapes with emphasis on flow separation (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armament Division, Air Force Systems Command, United States Air Force, 1983., 1983), by M. H. Clarkson, United States. Air Force. Systems Command, Air Force Armament Laboratory, and University of Florida. Department of Engineering Sciences (page images at HathiTrust)
• The Influence of high angle of attack flow pheomena on the dynamic stability of slender missiles (Eglin Air Force Base, Florida : Air Force Armament Laboratory, Armamaent Division, Air Force Systems Command, United States Air Force, 1983., 1983), by James M. Jenista, Robert C. Nelson, United States. Air Force. Systems Command, Air Force Armament Laboratory, and University of Notre Dame. |b Department of Aerospace and Mechanical Engineering (page images at HathiTrust)
• Two-component simultaneous LDV (Laser Doppler Velocimeter) turbulence measurements in an axisymmetric nozzle afterbody subsonic flow field with a cold, underexpanded supersonic jet (Arnold Air Force Base, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1983., 1983), by F. L. Heltsley, F. L. Crosswy, Calspan Field Services, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)
• A study of Dean vortex development and structure in a curved rectangular channel with aspect ratio of 40 at Dean numbers up to 430 (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1994), by Philip M. Ligrani, U.S. Army Research Laboratory, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• An oil flow study of a sonic reaction jet ejecting from a body of revolution into a free stream of Mach number range 1.75 to 4.5 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research and Development Directorate, Advanced Systems Labortory, 1970., 1970), by Troy A. Street, Redstone Arsenal (Ala.), and United States. Army. Missile Command. Research and Development Directorate (page images at HathiTrust)
• Correlation of viscous effects and comparison between experimental and theoretical distribution of potential normal force and pitching moment for bodies of revolution at supersonic speeds (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Research and Development Directorate, Advanced Systems Labortory, 1967., 1967), by William David Washington, Redstone Arsenal (Ala.), and United States. Army. Missile Command. Research and Development Directorate (page images at HathiTrust)
• Low-speed pressure measurements using a luminescent coating system (Stanford University, Dept. of Aeronautics and Astronautics, 2000), by Owen Clayton Brown, Stanford University. Dept. of Aeronautics and Astronautics, and Joint Institute for Aeronautics and Acoustics (page images at HathiTrust)

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