Dual mode Shock-Expansion/Reflected-Shock tunnel

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Erdos, John I ^a   Bakos, Robert J ^a   Castrogiovanni, Anthony ^a   Clayton Rogers, R ^b  

^a GASL ^*  (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AEROSPACE ENGINEERING; EXPANSION; FREE FLIGHT; MACH NUMBER; NASA; NOZZLES;

CALIBRATION DATA; CONVERGING-DIVERGING NOZZLES; DUAL-MODE OPERATION; FLIGHT CONDITIONS; FLIGHT SIMULATION; INTERFACE OPERATIONS; MODE OF OPERATIONS; TUNNEL OPERATION;

FLIGHT SIMULATORS;

EID: 84982318731     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

1. Bakos, R., Calleja, J., Erdos, J., Auslender, A., Sussman, M. and Wilson, G., "Design, Calibration and Analysis of a Tunnel Mode of Operation for the HYPULSE Facility," AIAA 96-219, New Orleans, LA, June 17-20, 1996.
2. Bakos, R., Calleja, J., Erdos, J., Sussman, M. and Wilson, G., "An Experimental and Computational Study Leading to New Test Capabilities for the HYPULSE Facility with a Detonation Driver," AIAA 96-219, New Orleans, LA, June 17-20, 1996.
3. Rausch, V, and Hunt, J., "NASA Hyper-X Program," Plenary Session Pap, AIAA 7th International Space Planes and Hypersonic Systems Conference, Norfolk, VA, Nov. 18-22, 1996.
4. Engers, R.J., Calleja, J.F., and Bakos, R.J., A Detonation Driven Injectant heater for Pulse Facility Testing Applications," AIAA 95-3153, July 1995.
5. Tsai, C-Y, Calleja, J.F., Bakos, R.J., and Rogers, R.C., "A Technique for Mixing Measurements in Hypervelocity Pulse Facilities Using Particle Scattering Imagery," AIAA 96-2222, June 1996.
6. Wang, L-G., Trucco, R.E., and Sachse, G.W., "Water Vapor Measurements for Combustion Diagnostics Using a 1350 nm Tunable Siode Laser," Presented at Laser Applications in Combustion and Combustion Diagnostics I, SPIE’s OE/LASE "94, January 22-29, 1994.
7. Miller, C.G. and Jones, J.J., "Development and Performance of the NASA Langley Research Center Expansion Tube/Tunnel; a Hypersonic-Hypervelocity Real-GAS Facility," Proc. 14 * Int’l Symp. On Shock Tubes and Wave, Sydney, Australia, August 15-18, 1983.
8. Mirels, H., "Test Time in Low Pressure Shock Tubes, Physics of Fluids, Vol. 6,№ 9, September 1963.
9. Erdos, J., Calleja, J., and Tamagno, J., "Increase in the Hypervelocity Test Envelope of the HYPULSE Shock-Expansion Tube," AIAA 94-2524, June 1994.
10. Wilson, G.J., Sussman, M.A., and Bakos, R.J., "Numerical Simulations of the Flow in the HYPULSE Expansion Tube," NASA TM-110357, June 1995.
11. Bakos, R.J., Castrogiovanni, A., Calleja, J.F., Nucci, L, and Erdos, J.I., "Expansion of the Scramjet Ground Testing Envelope of the HYPULSE Facility," AIAA 96-4506, November 1996.
12. Korte, J.J., and Hodge, J.S., "Flow Quality of Hypersonic Wind-Tunnel Nozzles Designed Using Computational Fluid Mechanics," Journal of Spacecrafted and Rocke, Vol. 32, №4, PP. 569-580, July-August 1995.
13. Guy, R.W., Rogers, R.C., Puster, R.L., Rock, K.E., and Diskin, G.S., "The NASA Langley Scramjet Test Complex," AIAA 96-324, July 1-3, 1996.