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ElectronicResource GovDoc
Author Prabhu, Ramadas K.

Title Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees [electronic resource] / Ramadas K. Prabhu.

Imprint Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:211267    ---  Available
Description 1 v.
Series [NASA contractor report] ; NASA/CR-2001-211267
NASA contractor report ; NASA CR-211267.
Note "December 2001."
Form Mode of access via the NASA web site.
Subject Aerodynamic characteristics.
Aerodynamic coefficients.
Angle of attack.
Computational fluid dynamics.
Hypersonic speed.
Inviscid flow.
Mach number.
Space shuttle orbiters.
Added Author Langley Research Center.
Gpo Item No. 0830-H-14 (online)
Sudoc No. NAS 1.26:211267

 
    
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