Thermostructural analysis of unconventional wing structures of a Hyper-X hypersonic flight research vehicle for the Mach 7 mission
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Author
Contributions
- Gong, Leslie. - Contributor
- Dryden Flight Research Facility. - Contributor
Publication
2001 - National Aeronautics and Space Administration, Dryden Flight Research Center, Edwards, Calif, California
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- Open LibraryOL16048424M
- OCLC Control Number51626927
Subjects
Topics
Wing panelsWing panels.Heat transferX wing rotorsHeat transfer.X wing rotors.Stress analysisStress analysis.Thermal bucklingThermal buckling.Temperature effectsStructural analysisHypersonic vehiclesStructural analysis.Hypersonic vehicles.Temperature effects.
Series Statement
- NASA/TP -- 2001-210398.
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