Airbreathing hypersonic vehicle design and analysis methods and interactions

Progress in Aerospace Sciences

Volumn 35, Issue 1, 1999, Pages 1-32

  Lockwood, Mary Kae ^a   Petley, Dennis H ^a   Martin, John G ^a   Hunt, James L ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

HYPERSONIC AERODYNAMICS; OPTIMIZATION;

AIRBREATHING HYPERSONIC VEHICLES;

SPACECRAFT;

EID: 0032733451     PISSN: 03760421     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0376-0421(98)00008-6     Document Type: Article

References (31)

1. Hunt JL. Hypersonic airbreathing vehicle design, hypersonics, vol I, Defining the hypersonic environment, Boston: Birkhauser, 1989.
2. Pinckney SZ, Walton JT. Program SRGULL: an advanced engineering model for the prediction of airframe-integrated subsonic/supersonic hydrogen combustion ramjet cycle performance. NASP TM-1120, January 1991.
3. Salas MD. Shock fitting method for complicated two-dimensional supersonic flows. AIAA J 1976; 14 (5).
4. Pinckney SZ. Isolator modeling for ramjet and ramjet/scramjet transition. National Aero-Space Plane Technology Review, Paper Number 171, 1993.
5. Weidner JP, Trexler CA, Emami S, Sullins G, McLafferty G, Azevedo D, Halenkamp M. Isolator development for E30. NASP Mid-Term Technology Review, Monterey, CA, 21-24 April 1992.
6. Bogar TJ, Alberico, JG, Johnson DB, Espinosa AM, Lockwood MK. Dual fuel lifting body configuration development. AIAA 96-4592, November 1996.
7. Spradley LW, Robertson SJ, Mahaffey WA, Lohner R. The solution adaptive modeling (SAM) CFD software system. RSI 96-002, September 1996.
8. Walters RW. GASP-A production level Navier-Stokes code including finite-rate chemistry. Proceedings of the Fourth Annual Meeting of the Center for Turbomachinery and Propulsion Research, April 1990.
9. Kamath PS, Mao M, McClinton CR. Scramjet combustor analysis with the SHIP3D PNS code. AIAA 91-5090, 1991.
10. Kamath PS, Mao M, McClinton CR. A parametric study of scramjet combustors for Mach 8 to Mach 20 flight. AIAA 91-1412, 1991.
11. Hunt JL, McClinton CR. Scramjet engine/airframe integration methodology. Paper C35, Presented at AGARD Conference Palaiseau, France, 14-16 April 1997.
12. Parametric Technology Corporation. Pro/ENGINEER Fundamentals, Parametric Technology Corporation, 1989-1994.
13. Bogar TJ, Eiswirth EA, Couch LM, Hunt JL, McClinton CR. Conceptual design of a Mach 10, global, reach reconnaissance aircraft, AIAA96-2894, 1996.
14. Lockwood MK et al. Design and analysis of a two-stage-to-orbit airbreathing hypersonic vehicle concept. AIAA 96-2890, 1996.
15. Collier C. Thermoelastic formulation of stiffened, unsymmetric composite panels for finite element analysis of high speed aircraft, AIAA 94-1579, 1994.
16. Collier C. Structural analysis and sizing of stiffened, metal matrix composite panels for hypersonic vehicles. AIAA 92-5015, 1992.
17. PDA Engineering. P3/PATRAN User Manual, vol. 1, Release 1.1A, PDA Engineering, Costa Mesa, CA, 1993.
18. The MacNeal-Schwedner Corporation, MSC/NASTRAN User's Manual, vol. 1, Version 68, The MacNeal-Schwedner Corporation, Los Angeles, CA, 1994.
19. Spradley LW, Robertson SJ, Mahaffey WA III, Armstrong WH, Lohner R, Collier CS. Solution-adaptive computer software for preliminary structural design of hypersonic vehicles. Final Report on Phase II SBIR NAS1-20423, 1997.
20. Bonner E, Clever W, Dunn K. Aerodynamic preliminary analysis system, part 1 theory. NASA CR-165628, 1981.
21. Engle CD, Praharaj SC. MINIVER upgrade for the AVID system, vol. I: LANMIN User's Manual. NASA CR-172212, 1983.
22. Cullimore BA et al, SINDA/FLUENT V 2.6 Reference Manual, 1994.
23. Petley DH, Jones SC, Dziedzic WM. Integrated numerical methods for hypersonic aircraft cooling systems analysis. AIAA Paper 92-0254, 1992.
24. Lau K. Boundary layer transition prediction method using APAS engineering code. NASP Memorandum, March 1993.
25. Elias T. Consensus X-30 boundary layer transition prediction method 'BLT-1A. NASP Coordination Memorandum No. 90-111, October 1990.
26. Emsley HT. I3G/VIRGO, interactive graphics for geometry generation and visual interactive rapid grid generation, User's Manual. WL-TM-91-316, June 1991.
27. I3G, Interactive graphics for geometry generation, User's Manual, vol. 1, AFWAL-TR-87-3064, 1987.
28. Advanced Technology Team. Access to space study, Final Report, vol. 3: Design Data. July 1993.
29. Brauer GL, et al. Program to optimize simulated trajectories (POST). NASA Contract NAS1-18147, September 1989.
30. Alberico JF. The development of an interactive computer tool for synthesis and optimization of hypersonic airbreathing vehicles. AIAA Paper 92-5076, 1992.
31. Design Synthesis, Inc. OptdesX-a software system for optimal engineering design Users Manual. Release 2.0.3, 1994.