An axisymmetric analog two-layer convective heating procedure with application to the evaluation of space shuttle orbiter wing leading edge and windeward surface heating
By: K.C. Wang.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- 188343.; NASA contractor report -- NASA CR-188343.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor]
Published: 1994
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic heatng.; Computational fluid dynamics.; Convective heat transfer.; Hypersonic heat transfer.; Inviscid flow.; Space shuttle orbiters.
Other titles: Axisymmetric analog two layer convective heating procedure with application to the evaluation of space shuttle orbiter wing leading edge and windeward surface heating.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0054-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.