Thermostructural analysis of unconventional wing structures of a Hyper-X hypersonic flight research vehicle for the Mach 7 mission
By: William L. Ko and Leslie Gong.
Contributors: Gong, Leslie.; Dryden Flight Research Facility.
Series: NASA/TP -- 2001-210398.; NASA technical paper -- 210398.
Publisher: National Aeronautics and Space Administration, Dryden Flight Research Center; Available from NASA Center for AeroSpace Information (CASI)
Published: 2001
Place of publication: Edwards, Calif; Hanover, MD
Language: eng
Format: Microform
Subjects: Hypersonic vehicles.; Temperature effects.; Structural analysis.; Stress analysis.; Heat transfer.; X wing rotors.; Wing panels.; Thermal buckling.
Notes: Shipping list no.: 2003-0098-M.

Also available via Internet from the NASA web site. Address as of 2/11/03: http://www.dfrc.nasa.gov/DTRS/2001/PDF/H-2453.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2002?] 1 microfiche.