Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions
By: William A. Wood.
Contributors: Langley Research Center.
Series: NASA/TM -- 1999-208998.; NASA technical memorandum -- 208998.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1999
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: X-34 reusable launch vehicle; Wind tunnel tests; Laminar boundary layer; Hypersonic heat transfer; Reynolds number; Turbulence effects; Aerothermodynamics; Turbulent boundary layer; Baldwin-Lomax turbulence model; Aerodynamic heating
Notes: Shipping list no.: 99-0471-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 1 microfiche.