Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees /

Bibliographic Details

Main Author:	Prabhu, Ramadas K.
Corporate Author:	Langley Research Center
Format:	Government Document Microform Book
Language:	English
Published:	Hampton, Va. : Hanover, MD : National Aeronautics and Science Administration, Langley Research Center ; Available from NASA Center for Aerospace Information, [2001]
Series:	NASA contractor report ; NASA CR-211267.
Subjects:	Aerodynamic characteristics. Aerodynamic coefficients. Angle of attack. COMPUTATIONAL FLUID DYNAMICS. Hypersonic speed. Inviscid flow. Mach number. Space shuttle orbiters.
Online Access:	https://purl.fdlp.gov/GPO/LPS39080