Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees
Title
Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees [microform] / Ramadas K. Prabhu.
Published by
Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
Also available via Internet from the NASA Web site. Address as of 2/21/04: http://techreports.larc.nasa.gov/ltrs/PDF/2001/cr/NASA-2001-cr211267.pdf; current access is available via PURL.
Reproduction (note)
Microfiche.
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 [microform] / Ramadas K. Prabhu.
Imprint
Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
Series
[NASA contractor report] ; NASA/CR-2001-211267
NASA contractor report ; NASA CR-211267.
Additional formats
Also available via Internet from the NASA Web site. Address as of 2/21/04: http://techreports.larc.nasa.gov/ltrs/PDF/2001/cr/NASA-2001-cr211267.pdf; current access is available via PURL.
Reproduction
Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2002?]. 1 microfiche.