Numerical simulation of high-speed civil transport inlet operability with angle of attack

AIAA Journal

Volumn 36, Issue 7, 1998, Pages 1223-1229

  Zha, Ge Cheng ^a,b   Knight, Doyle ^a   Smith, Donald ^c   Haas, Martín ^d,e  

^a RUTGERS UNIVERSITY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c RUTGERS UNIVERSITY   (United States)

^d UNITED TECHNOLOGIES RESEARCH CENTER   (United States)

^e AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0004237080     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.503     Document Type: Article

References (26)

1. Committee on Aeronautical Technologies, Aeronautical Technologies for the Twenty-First Century, National Research Council, National Academy Press, Washington, DC, 1992.
2. National Science and Technology Council, Goals for a National Partnership in Aeronautics Research and Technology, Executive Office of the President of the United States, Washington, DC, 1995.
3. Saunders, J., and Keith, T., "Results from Computational Analysis of a Mixed Compression Supersonic Inlet," AIAA Paper 91-2581, June 1991.
4. Hamed, A., and Lehnig, T., "An Investigation of Oblique Shock/Boundary Layer Bleed Interaction," AIAA Paper 90-1928, July 1990.
5. Cooper, G., and Sirbaugh, J., "PARC Code: Theory and Usage," Arnold Engineering Development Center, AEDC-TR-89-15, Arnold AFB, TN, 1989.
6. Slater, J. W., Chung, J., and Cole, G. L., "Computation of Unsteady Aeropropulsion Flows with Moving Geometry," Proceedings of 1st Air Force Office of Scientific Research Conference on Dynamic Motion CFD, Rutgers Univ., Piscataway, NJ, 1996, pp. 271-279.
7. Mayer, D., and Paynter, G. C., "Prediction of Supersonic Inlet Unstart Caused by Freestream Disturbances," AIAA Journal, Vol. 33, No. 2, 1995, pp. 266-275.
8. Mayer, D., and Paynter, G. C., "Boundary Conditions for Unsteady Supersonic Inlet Analyses," AIAA Journal, Vol. 32, No. 6, 1994, pp. 1200-1206.
9. Slater, J. W., "Efficient Computation of Unsteady Planar Internal Viscous Flows with Moving Geometry," AIAA Paper 96-0113, Jan. 1996.
10. Neaves, M. D., and McRae, D. S., "Numerical Investigations of Axisymmetric and Three-Dimensional Supersonic Inlet Flow Dynamics Using a Solution Adaptive Mesh," Proceedings of 1st Air Force Office of Scientific Research Conference on Dynamic Motion CFD, Rutgers Univ., Piscataway, NJ, 1996, pp. 235-243.
11. Benson, R. A., and McRae, D. S., "A Three-Dimensional Dynamic Solution-Adaptive Mesh Algorithm," AIAA Paper 90-1566, 1990.
12. Goble, B. D., King, S., Terry, J., and Schoop, M., "Inlet Hammershock Analysis Using a 3-D Unsteady Euler/Navier-Stokes Code," AIAA Paper 96-2547, July 1996.
13. Miller, D. N., and Smith, B. R., "Time-Dependent CFD Analysis of Inlet Unstart," Proceedings of 1st Air Force Office of Scientific Research Conference on Dynamic Motion CFD, Rutgers Univ., Piscataway, NJ, 1996, pp. 291-297.
14. Vadyak, J., Hoffman, J., and Bishop, A. R., "Calculation of the Flow Field in Supersonic Mixed-Compression Inlets at Angle of Attack Using the Three-Dimensional Method of Characteristics with Discrete Shock Wave Fitting," NASA CR-135425, 1978.
15. Howlett, D. G., and Hunter, L., "A Study of a Supersonic Axisymmetric Spiked Inlet at Angle of Attack Using the 3-D Navier-Stokes Equations," AIAA Paper 86-0308, Jan. 1986.
16. Bowditch, D. N., "Some Design Considerations for Supersonic Cruise Mixed Compression Inlets," NASA TM-X-71460, 1973.
17. Wasserbauer, J. F., Shaw, R. J., and Neumann, H. E., "Design of a Very-Low-Bleed Mach 2.5 Mixed-Compression Inlet with 45 Percent Internal Contraction," NASA TM X-3135, March 1975.
18. Wasserbauer, J. F., Neumann, H. E., and Shaw, R. J., "Distortion in a Full-Scale Bicone Inlet with Internal Focused Compression and 45 Percent Internal Contraction," NASA TM-X-3133, Dec. 1974.
19. Wasserbauer, J. F, Neumann, H. E., and Shaw, R. J., "Performance and Surge Limits of a TF30-P-3 Turbofan Engine/Axisymmetric Mixed-Compression Inlet Propulsion System at Mach 2.5," NASA TP-2461, May 1985.
20. Zha, G.-C., Smith, D., Schwabacher, M., Rasheed, K., Gelsey, A., and Knight, D., "High Performance Supersonic Missile Inlet Design Using Automated Optimization," Journal of Aircraft, Vol. 34, No. 6, 1997, pp. 697-705.
21. "GASP v3 User's Manual," Aerosoft, Inc., May 1996.
22. Mizukami, M., and Saunders, J., Parametrics on 2D Navier-Stokes Analysis of a Mach 2.68 Bifurcated Rectangular Mixed-Compression Inlet," NASA TM-107003, July 1995.
23. Zha, G.-C., Knight, D., Smith, D., and Haas, M., "Numerical Simulation of HSCT Inlet Operability with the Angle of Attack," AIAA Paper 97-2761, July 1997.
24. Chyu, W., Howe, G., and Shih, T. L-P, "Bleed Boundary Conditions for Numerically Simulated Mixed-Compression Supersonic Inlet Flow," Journal of Propulsion and Power, Vol. 8, No. 4, 1992, pp. 862-868.
25. Shlh, T. I.-P., Rimlinger, M., and Chyu, W., "Three-Dimensional Shock-Wave/Boundary-Layer Interactions with Bleed," AIAA Journal, Vol. 31, No. 10, 1993, pp. 1819-1826.
26. Zha, G.-C., Knight, D., and Smith, D., "Numerical Investigations of HSCT Inlet Unstart Transient at Angle of Attack," AIAA Paper 98-3583, July 1998.