Metallic thermal protection system panel flutter study

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Chen, Roger R ^a   Blosser, Max L ^b  

^a LOCKHEED MARTIN   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

HEAT SHIELDING; HYPERSONIC VEHICLES; METALS; REUSABILITY; THERMAL INSULATING MATERIALS;

AEROELASTIC VIBRATION; ANALYSIS CAPABILITIES; COMMERCIAL FINITE ELEMENT CODES; EXPERIMENTAL VEHICLE; METALLIC THERMAL PROTECTION SYSTEM; REUSABLE LAUNCH VEHICLES; STRUCTURAL NON-LINEARITIES; UNSTEADY AERODYNAMICS;

FLUTTER (AERODYNAMICS);

EID: 85016051104     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-501     Document Type: Conference Paper

References (10)

1. Blosser, M. L., "Advanced Metallic Thermal Protection Systems for Reusable Launch Vehicles", Ph. D. Dissertation, UVA, May 2000.
2. Mclntosh, S. G., Jr., "Theoretical Considerations of Some Nonlinear Aspects of Hypersonic Panel Flutter, " Dept. of Aeronautics and Astronautics, Stanford Univ., Final Rept, Sept. 1, 1965 to Aug. 31, 1970; SUDAARNo. 491.
3. Gray, C. E., Jr., and Mei, C., "Large Amplitude Finite Element Flutter Analysis of Composite Panel in Hypersonic Flow, " AIAA Journal, Vol. 31, No. 6, 1993, pp. 1090-1099.
4. Bein, T., Friedmann, P., Zhong, X. and Nydick, L, " Hypersonic flutter of a curved shallow panel with aerodynamic heating, " 34th Structures, Structural Dynamics and Materials Conf., La Jolla, CA, 1993.
5. Abdel-Motaglay, K., Chen, R. and Mei, C., "Nonlinear Flutter of Composite Panels Under Yawed Supersonic Flow Using Finite Elements", AIAA Journal, Vol. 37, No. 9,1999, pp. 1025-1032.
6. Xue, D. Y. X, "Finite Element Frequency Domain Solution of Nonlinear Panel Flutter with Temperature Effects and Fatigue Life Analysis" Ph. D. Dissertation, Dept. of Aerospace Engineering, Old Dominion Univ. Norfolk, VA, 1991.
7. MARC Analysis Research Corporation, "User Manual", Palo Alto, CA, 1994.
8. Ashley, H. and Zartarian, G., "Piston theory-a new aerodynamic tool for aeroelastician", Journal of Aeronautical Science, Vol. 23, No. 12, 1956, pp.1109-1118.
9. BF Goodrich Inc. Private communication, October 1997.
10. Sawyer, J. W., Hodge, J. S., Moore B. and Sawyer K., "Aerothermal Test of Thermal Protection Systems for X-33 Reusable Launch Vehicle", Space Technology and Applications International Forum (STAIF '99), Albuquerque, New Mexico, January 31-February 4, 1999.