Books on the topic 'Hypersonic wind tunnels'

Jacobi, L. Y. I.A.I. hypersonic wind tunnel. Ben Gurion Airport, Israel: Israel Aircraft Industries Ltd, 1987.

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

Lee, J. Lawrence. Into the wind: The wind tunnels of NASA and its predecessors. Washington, DC: National Aeronautics and Space Administration, Office of Communications, History Program Office, 2012.

Lu, Frank K. Survey of short duration, hypersonic and hypervelocity facilities. Washington, D. C: American Institute of Aeronautics and Astronautics, 1994.

Norris, R. B. The flying wind tunnel. New York: AIAA, 1989.

K, Lu Frank, and Marren Dan E, eds. Advanced hypersonic test facilities. Reston, Va: American Institute of Aeronautics and Astronautics, 2002.

Midden, Raymond E. Description and calibration of the Langley hypersonic CF: A facility for simulating low ©. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

Midden, Raymond E. Description and calibration of the Langley hypersonic CF: A facility for simulating low. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

F, Akyurtlu Ates, and United States. National Aeronautics and Space Administration., eds. Evaluation of candidate working fluid formulations for the electrothermal-chemical wind tunnel: Final report for NAG-1-767. [Hampton, Va.]: Hampton University, Dept. of Engineering, 1993.

Haas, Jeffrey E. Reactivation study for NASA Lewis Research Center's Hypersonic Tunnel Facility. [Washington, DC: National Aeronautics and Space Administration, 1987.

R, Mielke Roland, Langley Research Center, Old Dominion University. Research Foundation., and Old Dominion University. Dept. of Electrical Engineering., eds. Ultrasound instrumentation for the 7" Mach Seven Tunnel: Final report for the period August 28, 1984 to December 31, 1984. Norfolk, Va: Dept. of Electrical Engineering, School of Engineering, Old Dominion University, 1985.

Thompson, R. A. Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF?□Tunnel. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

Thompson, R. A. Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987.

R, Mielke Roland, Langley Research Center, Old Dominion University. Research Foundation., and Old Dominion University. Dept. of Electrical Engineering., eds. Ultrasound instrumentation for the 7" Mach Seven Tunnel: Final report for the period August 28, 1984 to December 31, 1984. Norfolk, Va: Dept. of Electrical Engineering, School of Engineering, Old Dominion University, 1985.

Simeonides, G. The performance of the VKI Longshot hypersonic wind tunnel. Rhode Saint Genese, Belgium: von Karman Institute for Fluid Dynamics, 1987.

A, Thompson Richard. Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF4 Tunnel. Hampton, Va: Langley Research Center, 1987.

Simeonides, G. The VKI hypersonic wind tunnels and associated measurement techniques. Rhode Saint Genese, Belgium: von Karman Institute for Fluid Dynamics, 1990.

Center, NASA Glenn Research, ed. Plumbrook Hypersonic Tunnel Facility graphite furnace degradation mechanisms. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Sprinkle, Danny R. Langley 8-ft. HTT test 139 gas analyses. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Sprinkle, Danny R. Langley 8-ft. HTT test 139 gas analyses. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

P, Davis Patricia, and Langley Research Center, eds. Langley 8-ft. HTT test 139 gas analyses. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Sprinkle, Danny R. Langley 8-ft. HTT test 139 gas analyses. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Sprinkle, Danny R. Langley 8-ft. HTT test 139 gas analyses. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Sprinkle, Danny R. Langley 8-ft. HTT test 139 gas analyses. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Tamagno, Jose. Hypervelocity real gas capabilities of GASL's expansion tube (HYPULSE) facility. Washington, D. C: American Institute of Aeronautics and Astronautics, 1990.

G, Fletcher Douglas, and Ames Research Center, eds. Laser-spectroscopic measurement techniques for hypersonic, turbulent wind tunnel flows. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

G, Fletcher Douglas, and Ames Research Center, eds. Laser-spectroscopic measurement techniques for hypersonic, turbulent wind tunnel flows. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1992.

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.

Rood, Robert. Mach 5 electroformed nickel nozzle refurbishment: FNAS investigation of ultra-smooth surfaces. [Washington, DC: National Aeronautics and Space Administration, 1992.

Lyndon B. Johnson Space Center. Systems Engineering Division. and Chrysler Corporation. Electronics Products Division. Michoud Engineering Office. Data Management Services., eds. Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42). Houston, Tex: Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, 1985.

C, Stanton Alan, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Nonintrusive fast response oxygen monitoring system for high temperature flows. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Lyndon B. Johnson Space Center. Systems Engineering Division. and Chrysler Corporation. Electronics Products Division. Michoud Engineering Office. Data Management Services., eds. Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42). Houston, Tex: Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, 1985.

Miller, C. G. Hypersonic aerodynamic/aerothermodynamic testing capabilities at Langley Research Center. Washington: AIAA, 1992.

United States. National Aeronautics and Space Administration., ed. Design and Navier-Stokes analysis of hypersonic wind tunnel nozzles. [Washington, DC: National Aeronautics and Space Administration], 1989.

George C. Marshall Space Flight Center., ed. Application of rapid prototyping methods to high-speed wind tunnel testing (MSFC Center Director's Discretionary Fund final report, project no. 96-21). [Huntsville, Ala.]: National Aeronautics and Space Administration, Marshall Space Flight Center, 1998.

Peñaranda, Frank E. Aeronautical facilities catalogue. Washington, DC: Scientific and Technical Information Branch, National Aeronautics and Space Administration, 1985.

Peñaranda, Frank E. Aeronautical facilities catalogue. Washington, DC: Scientific and Technical Information Branch, National Aeronautics and Space Administration, 1986.

Peñaranda, Frank E. Aeronautical facilities catalogue. Washington, DC: Scientific and Technical Information Branch, National Aeronautics and Space Administration, 1985.

Peñaranda, Frank E. Aeronautical facilities catalogue. Washington, DC: Scientific and Technical Information Branch, National Aeronautics and Space Administration, 1985.

Roane, Hunt L., Prabhu Ramadas K, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Roane, Hunt L., Prabhu Ramadas K, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

W, Kniskern Marc, Monta William J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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.

W, Kniskern Marc, Monta William J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

Center, Langley Research, ed. Simultaneous luminescence pressure and temperature measurement system for hypersonic wind tunnels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Lyndon B. Johnson Space Center. Systems Engineering Division. and Chrysler Corporation. Electronics Products Division. Michoud Engineering Office. Data Management Services., eds. Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A&C (IH-97A/B/C). Houston, Tex: Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, 1985.

W, Paulson John, Weilmuenster K. James, and United States. National Aeronautics and Space Administration., eds. Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly. Washington, DC: American Institute of Aeronautics and Astronautics, 1995.

Center, Langley Research, ed. Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Center, Langley Research, ed. Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Center, Langley Research, ed. Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.