Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly
By: Gregory J. Brauckmann; John W. Paulson, Jr.; K. James Weilmuenster.
Contributors: Paulson, John W.; Weilmuenster, K. James.; United States. National Aeronautics and Space Administration.
Series: NASA-TM -- 112155.; NASA technical memorandum -- 112155.
Publisher: American Institute of Aeronautics and Astronautics; [National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Space shuttle orbiters.; Wind tunnel tests.; Hypersonic wind tunnels.; Pitching moments.; Temperature effects.; Flow distribution.; Gas flow.; Ideal gas.; Navier-Stokes equation.
Notes: Shipping list no.: 98-0810-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.