Summary report of the orbital X-34 wing static aeroelastic study
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Author
Contributions
- Langley Research Center. - Contributor
Publication
2001 - National Aeronautics and Science Administration, Langley Research Center, Hampton, Va, Virginia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- OCLC Control Number50133893
- Open LibraryOL17607405M
Subjects
Topics
Free flowFlexibilityInviscid flowAeroelasticityDynamic pressureAerodynamic characteristicsX-34 reusable launch vehicleComputational fluid dynamics
Series Statement
- [NASA contractor report] -- NASA/CR-2001-210850.
- NASA contractor report -- NASA CR-210850.
Other Editions
- Summary report of the orbital X-34 wing static aeroelastic study
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