Books on the topic 'Flow studies in wind tunnels'

Christopoulos, George P. Oscillating-flow wind tunnel studies for a circulation control circular cylinder. Monterey, Calif: Naval Postgraduate School, 1991.

Lederer, Melissa A. Condensation in hypersonic nitrogen wind tunnels. Washington: American Institute of Aeronautics and Astronautics, 1990.

Everhart, Joel L. Slotted-wall flow-field measurements in a transonic wind tunnel. Hampton, Va: Langley Research Center, 1991.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. Hampton, Va: Langley Research Center, 1989.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. Washington D.C: National Aeronautics and SpaceAdministration, 1989.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Asai, Keisuke. Hot-jet simulation in cryogenic wind tunnels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Development, North Atlantic Treaty Organization Advisory Group for Aerospace Research and. Boundary layer simulation and control in wind tunnels. Neuilly sur Seine, France: AGARD, 1988.

Gentry, Garl L. The Langley 14- by 22-foot subsonic tunnel: description, flow characteristics, and guide for users. Hampton, Va: Langley Research Center, 1990.

Newton, James E. Icing of flow conditioners in a closed-loop wind tunnel. [Washington, DC: National Aeronautics and Space Administration, 1987.

Newton, James. Icing of flow conditioners in a closed-loop wind tunnel. [Washington, DC: National Aeronautics and Space Administration, 1987.

West, James W. A System to measure flow moisture content in hypersonic wind tunnels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Mabey, Dennis G. Further buffeting tests in a cryogenic wind tunnel. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Brooks, Cuyler W. The NASA Langley 8-Foot Transonic Pressure Tunnel calibration. Hampton, Va: Langley Research Center, 1994.

Brooks, Cuyler W. The NASA Langley 8-foot transonic pressure tunnel calibration. Hampton: National Aeronautics and Space Administration, Langley Research Center, 1994.

Boldman, Donald R. Experimental evaluation of two turning vane designs for fan drive corner of 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel. Cleveland, Ohio: Lewis Research Center, 1987.

Capone, Francis J. The NASA Langley 16-Foot Transonic Tunnel: Historical overview, facility description, calibration, flow characteristics, and test capabilities. Hampton, Va: Langley Research Center, 1995.

Schneider, Steven P. A quiet flow Ludwieg tube for study of transition in compressible boundary layers: Design and feasibility. West Lafayette, IN: School of Aeronautics and Astronautics, Purdue University, 1991.

Gobert, J. Preliminary study of an apparatus to control the temperature of the flow entering the T2 cryogenic wind tunnel. Washington, DC: National Aeronautics and Space Administration, 1987.

Bell, J. H. Contraction design for small low-speed wind tunnels. [Washington, DC: National Aeronautics and Space Administration, 1988.

EURASAP International Workshop on Wind and Water Tunnel Modelling of Atmospheric Flow and Dispersion (6th 1993 Aso, Japan). 6th EURASAP International Workshop on Wind and Water Tunnel Modelling of Atmospheric Flow and Dispersion: Aso, Japan, 25-27 August 1993, plus regular papers. Oxford: Pergamon, 1996.

Moore, Royce D. Detailed flow surveys of turning vanes designed for a 0.1-scale model of NASA Lewis Research Center's proposed altitude wind tunnel. Cleveland, Ohio: Lewis Research Center, 1987.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Boundary layer simulation and control in wind tunnels: Report of the fluid dynamics panel working group 09. S.l: s.n, 1988.

Erickson, Gary E. Fiber-optic-based laser vapor screen flow visualization sysytem for aerodynamic research in larger scale subsonic and transonic wind tunnels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Erickson, Gary E. Fiber-optic-based laser vapor screen flow visualization sysytem for aerodynamic research in larger scale subsonic and transonic wind tunnels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Dress, David A. Computer program for calculating flow parameters and power requirements for cryogenic wind tunnels. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Huebner, Lawrence D. Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation. Hampton, Va: Langley Research Center, 1993.

Bruce, Robert A. A vapor generator for transonic flow visualization. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

Bruce, Robert A. A vapor generator for transonic flow visualization. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

Bowcutt, K. G. The use of panel methods for the development of low subsonic wall interference and blockage corrections. New York: AIAA, 1985.

Hollis, Brian R. Real-gas flow properties for NASA Langley Research Center Aerothermodynamics Facilities Complex wind tunnels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

T, Pickett Mark, Sheldon David W, and United States. National Aeronautics and Space Administration., eds. Flow quality studies of the NASA Lewis Research Center Icing Research Tunnel. [Washington, D.C.]: National Aeronautics and Space Administration, 1994.

Experimental studies of transonic flow field near a longitudinally slotted wind tunnel wall. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

T, Pickett Mark, Sheldon David W, and United States. National Aeronautics and Space Administration., eds. Flow quality studies of the NASA Lewis Research Center Icing Research Tunnel diffuser. [Washington, DC]: National Aeronautics and Space Administration, 1994.

T, Pickett Mark, and United States. National Aeronautics and Space Administration., eds. Flow quality studies of the NASA Lewis Research Center 8- by 6-foot supersonic/9- by 15-foot low speed wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, 1992.

C, Gonsalez Jose, Kee-Bowling Bonnie A, and NASA Glenn Research Center, eds. Flow quality studies of the NASA Glenn Research Center Icing Research Tunnel circuit (1995 tests). [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2000.

Experimental studies of shock-wave/wall-jet interaction in hypersonic flow. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Boundary layer transition studies: November 1990 to February 1995. San Jose, CA: MCAT Institute, 1995.

Jan, Lepicovsky, and United States. National Aeronautics and Space Administration., eds. A supersonic tunnel for laser and flow-seeding techniques. [Washington, D.C.]: National Aeronautics and Space Administration, 1994.

B, Igoe William, Flechner Stuart G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Slotted-wall flow-field measurements in a transonic wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

Slotted-wall flow-field measurements in a transonic wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

B, Igoe William, Flechner Stuart G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, eds. Slotted-wall flow-field measurements in a transonic wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

Slotted-wall flow-field measurements in a transonic wind tunnel. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

Engineers, Society of Automotive, ed. Aerodynamic flow visualization techniques and procedures. Warrendale, PA: Society of Automotive Engineers, 1986.

United States. National Aeronautics and Space Administration., ed. A study of juncture flow in the NASA Langley 0.3-meter transonic cryogenic tunnel. [Washington, DC: National Aeronautics and Space Administration, 1992.

Improvement in the quality of flow visualization in the Langley 0.3-meter transonic cryogenic tunnel. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.