Design, fabrication, and calibration of a mach 6.5 hypersonic shock tunnel nozzle for scramjet testing applications

20th AIAA Advanced Measurement and Ground Testing Technology Conference

Volumn , Issue , 1998, Pages

  Modroukas, Dean ^a   Betti, Alexander ^a   Chinitz, Wallace ^a   Bakos, Robert ^a  

^a GASL Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CALIBRATION; FABRICATION; NAVIER STOKES EQUATIONS; SHOCK TESTING; TUNNELS;

AERODYNAMIC SIMULATIONS; COMPUTATIONAL SIMULATION; FLIGHT CONDITIONS; HIGH RESOLUTION; MATERIAL SELECTION; NOZZLE EXIT PLANE; PARABOLIZED NAVIER-STOKES (PNS); SCRAMJET TESTING;

NOZZLE DESIGN;

EID: 85085406389     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-2496     Document Type: Conference Paper

References (9)

1. Erdos, J.I., Bakos, R.J., Castrogiovanni, A., and Rogers, R.C.," Dual Mode Shock- Expansion/Reflected-Shock Tunnel," AIAA Paper 97-0560, January 1997.
2. Bakos, R.J., Castrogiovanni, A., Calleja, J.F., Nucci, L, and Erdos, J.I., "Expansion of the Scramjet Ground Test Envelope of the HYPULSE Facility," AIAA Paper 96-4506, November, 1996.
3. Tsai, C.Y., Calleja, J.F., and Bakos, R.J., "Shock-Tunnel Flow Visualization with a High- Speed Schlieren and Laser Holographic Interferometry System," AIAA Paper 98-2700, June 1998.
4. Lukasiewicz, J., "Experimental Methods of Hypersonics," Marcel Dekker, Inc., New York, 1973.
5. McClinton, C.R., Holland, S.D., Rock, K.E., Engelund, W.C., Voland, R.T., Huebner, L.D., and Rogers, R.C., "Hyper-X Wind Tunnel Program," AIAA Paper 98-0553, January 1998.
6. GASP Version 3 - The General Aerodynamic Simulation Program USER'S Manual. Aerosoft, Inc., Blacksburg, VA, 1996.
7. Korte, J.J, and Hodge, J.S., "Flow Quality of Hypersonic Wind-Tunnel Nozzles Designed Using Computational Fluid Dynamics," Journal of Spacecraft and Rockets, Vol. 32, No. 4, 1995, pp 569-580.
8. Chadwick, K.M., Holden, M.S., Korte, J.J., and Anderson, E.G., "Design and Fabrication of a Mach 8 Contoured Nozzle for the LENS Facility," AIAA Paper 96-0585, January 1996.
9. Baldwin, B.S., and Lomax, H., "Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows," AIAA Paper 78-0257, January 1978.