Hyper-X hot structures design and comparison with flight data

A Collection of Technical Papers - 13th AIAA/CIRA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn 3, Issue , 2005, Pages 2084-2098

  Leonard, C P ^a,b,c   Amundsen, R M ^a,c,d   Bruce III, W E ^a,c,d  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Exploration Concepts Branch   (United States)

^c AIAA   (United States)

^d Structural and Thermal Systems Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT DATA; HOT STRUCTURES; SCRAMJETS; THERMAL ENVIRONMENT;

DATA RECORDING; DATA REDUCTION; RISK ASSESSMENT; THERMOANALYSIS; THERMOCOUPLES;

FLIGHT DYNAMICS;

EID: 29144510464     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. Amundsen R. M., Leonard, C. P., and Torres, A. O., "Thermal Analysis of the Hyper-X Research Vehicle Wing, Mach 7 Design," presented at the 97 JANNAF Conference, Chemical Propulsion Information Agency, West Palm Beach, Florida, October 1997.
2. Amundsen, R. M., Comparison of Integrated Analysis Methods for Two Model Scenarios, Ninth Conference, Workshop and Product Presentation on Thermal and Fluids Analysis Tools and Methods, Cleveland, Ohio, August-September, 1998.
3. Amundsen, R. M., "Method Improvements in Thermal Analysis of Mach 10 Leading Edges," presented at the Tenth Conference, Workshop and Product Presentation on Thermal and Fluids Analysis Tools and Methods, NASA Huntsville, AL September 1999.
4. Amundsen R. M., and Brzowski, M., "Correlation of Thermal Model with Hyper-X Leading Edge Material Testing," presented at the 25th Annual Conference on Composites, Materials and Structures, Cocoa Beach, Florida, January 2001.
5. Amundsen, R. M., and Leonard, C. P., "Hypersonic Thermal Analysis including Shock Interaction Load Amplification with Motion Effects", 27th Annual Conference on Composites, Materials and Structure, January 2003, Cocoa Beach, Florida.
6. Amundsen, R. M., Bruce, W. E., Leonard, C. P., "Hyper-X Hot Structures Comparison of Thermal Analysis and Flight Data", 15th Thermal & Fluid Analysis Workshop (TFAWS 04), Pasadena, California, August-September 2004.
7. Leonard, C. P., and Cuda, V., "Aerothermal Analysis in a Rapid Prototyping Environment", 36th CS/APS JANNAF Conference, Cocoa Beach, FL, October 1999.
8. Lindell, M. C., and Amundsen, R. M., "Nonlinear Thermal/Structural Analysis of Hypersonic Vehicle Hot Structures", presented at the NASA Workshop on Innovative Finite Element Solutions to Challenging Problems, NASA GSFC, May 2000.
9. Gentry, A. E., Smith, G. N., Wayne, O., The Mark IV Supersonic Arbitrary Body Program, AFFDL-TR-73-159, Volumes I, II & III, November 1973.
10. MSC/PATRAN User Manual, MacNeal-Schwendler Corporation, Version 2000 (r2), August 2000.