Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
By: Jim A. Penland and Richard Hawkins.
Contributors: Hawkins, Richard.; Langley Research Center.
Series: NASA technical paper -- 3673.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1997
Place of publication: Hampton, Va; Springfield, VA
Language: eng
Format: Microform
Subjects: Hypersonic shock.; Hypersonic boundary layer.; Hypersonic forces.; Turbulent boundary layer.; Reynolds number.; Mach number.; Computational fluid dynamics.; Body-wing configurations.; Aerodynamic drag.; Aerodynamic coefficients.
Notes: Shipping list no.: 1999-0723-M.

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