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Nas 1. 26 :211267
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Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 de


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

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 Axe Federal Documents Online  NAS 1.26:211267    ---  Available
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E-Book/E-Doc
 

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


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

Rating:

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:211267    ---  Available
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