Aeroheating predictions for X-34 using an inviscid-boundary layer method
By: Christopher J. Riley and William L. Kleb, Steven J. Alter.
Contributors: Kleb, William L.; Alter, Steven J.; United States. National Aeronautics and Space Administration.
Series: [NASA technical memorandum] -- 207288.; NASA technical memorandum -- 207288.
Publisher: American Institute of Aeronautics and Astronautics; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1998
Place of publication: Reston, VA; [Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Subjects: Inviscid flow.; Boundary layers.; X-34 reusable launch vehicle.; Surface temperature.; Turbulent flow.; Convective heat transfer.; Aerodynamic heating.; Algorithms.
Notes: Shipping list no.: 99-0199-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.