Hypersonic aerothermodynamics/aerothermoelastics methodology for reusable launch vehicles/TPS design and analysis

41st Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2003, Pages

  Liu, D D ^a,b   Chen, P C ^a   Tang, L ^a   Chang, K T ^a  

^a ZONA TECHNOLOGY INC   (United States)

^b ARIZONA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CODES (SYMBOLS); COMPUTATIONAL FLUID DYNAMICS; LAUNCH VEHICLES; LAUNCHING; REUSABILITY; REUSABLE ROCKETS; SOFTWARE TESTING; STRUCTURAL OPTIMIZATION; THERMODYNAMICS; TRAJECTORIES;

DESIGN AND ANALYSIS; EXTREME ENVIRONMENT; MULTIDISCIPLINARY DESIGN OPTIMIZATION; OPTIMIZATION SOFTWARE; RE-USABLE LAUNCH VEHICLES (RLV); REUSABLE LAUNCH VEHICLES; THERMAL PROTECTION SYSTEM; TRAJECTORY ANALYSIS;

HYPERSONIC VEHICLES;

EID: 85086491887     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-897     Document Type: Conference Paper

References (21)

1. Liu, D. D., Chen, P. C., Tang, L., Chang, K. T., Chemaly, A. and Kamhawi, H., Integrated Hypersonic Aerothermoelastic Methodology for Transatmospheric Vehicle (TAV)/Thermal Protection System (TPS) Structural Design and Optimization, AFRL-VA-WP-TR-2002-3047, January, 2002.
2. Freemanm D.C., Jr., Talay, T.A., and Austin, R.E., Reusable Launch Vehicle Technology Program. IAF96-V.4.01, Oct. 1996.
3. Hamilton, H. H., De Jarnette, F. R., and Weilmuenster, K. J., Approximate Method for Calculating Heating Rates on Three-Dimensional Vehicles, Journal of Spacescraft and Rockets, Vol. 31, No. 3, 1994, pp. 345.354.
4. Johnson, E.H. and Venkayya V.B., Automated Structural Optimization System (ASTROS), Theoretical, User. s, Application. s, Programmer. s Manual, AFWAL-TR-88-3028, Vol. I-IV, Dec. 1998.
5. The Adaptive Modeling Language, TECHNOSOFT, Inc., Copyright 1993-1999, www.technosoft.com
6. Bonner, E., Clever, W., and Dunn, K., "Aerodynamic Preliminary Analysis System II Part I. Theory". NASA CR 182076, Apr. 1991.
7. Hoak, D. E., and Finck, R. D., USAF Stability and Control Datcom, Vol. 1-4, Air Force Wright Aeronautical Labs., Apr. 1978.
8. Moore, F. G., Mcinville, R. M., and Hymer, T., The 1998 Version of the NSWC Aeroprediction Code: Part I. Summary of New Theoretical Methodology, NSWCDD/TR-98/1, Apr. 1998.
9. Krist, S.L., Biedron, R.T., and Rumsey, C.L., CFL3D User. s Manual. NASA Langley Research Center, 1997.
10. Burns, K.A., Deters, K.J., Haley, C.P., Kihlken, T.A., Viscous Effects on Complex Configurations. WL-TR-95-3059, 1995.
11. Chen, P.C. and Liu, D.D. Unified Hypersonic/Supersonic Panel Method for Aeroelastic Applications to Arbitrary Bodies, Journal of Aircraft, Vol. 39, No. 3, May-June 2002.
12. Chen, P.C. and Liu, D.D. Hypersonic Aerodynamic Analysis of Bent-Nose CKEM Body Using ZAERO, Army MRDEC/Dynetics Contract Report (ZONA Rpt 00-40) Oct. 2000.
13. Chen, P.C. and Liu, D.D., ZONAIR: A Finite-Element Based Aerodynamic/Loads System Using a Unified High-Order Sub/Super/Hypersonic Panel Methodology, Presented at Aerospace Flutter and Dynamics Council, May 8-10, 2002, Sedona, AZ.
14. White, F.M., Viscous Fluid Flow, McGraw Hill, Inc. 1974.
15. Hamilton, H.H., DeJarnette, F.R., and Weilmuenster, K.J., Application of Axisymmetric Analogy for Calculating Heating in Three-Dimensional Flows. Journal of Spacecraft, Vol. 24, No. 4, July-August 1987.
16. Engel, C.D., and Schmitz, C.P., MINIVER Upgrade for the AVID System., Vol. 3, EXITS User. s and Input Guide, NASA CR-172214, Aug. 1983.
17. Myers, D.E., Martin, C.J. and Blosser, M.L., Parametric Weight Comparison of Advanced Metallic, Ceramic Tile, and Ceramic Blanket Thermal Protection Systems, NASA TM 2000-210289.
18. Riley, C.J. and DeJarnette, F.R., Engineering Aerodynamic Heating Method for Hypersonic Flow, Journal of Spacecraft and Rockets, Vol. 29, No. 3, May-June 1992.
19. Johnson, E.H. and Venkayya, V.B., Automated Structural Optimization System (ASTROS), Theoretical Manual., AFWAL-TR-88-3028, Vol. 1, December 1988.
20. Chen, P.C., Liu, D.D., Sarhaddi, D., Striz, A.G., Neill, D.J., and Karpel, M., Enhancement of the Aeroservoelastic Capability in ASTROS, STTR Phase I Final Report, WL-TR-96-3119, Sep. 1996.
21. Chen, P.C., Sarhaddi, D., and Liu, D.D., Development of the Aerodynamic/ Aeroservoelastic Modules in ASTROS, ZAERO User. s/Programmer. s/Applications/ Theoretical Manuals, AFRL-VA-WP-TR-1999-3049/3050/3051/3052, Feb. 1999.