Showing 1 - 10 results of 10 for search 'Prabhu, Ramadas K.', query time: 0.12s Refine Results
  1. 1
    An inviscid computational study of an X-33 configuration at hypersonic speeds /
    by Prabhu, Ramadas K.
    Published 1999
    Government Document Book
  2. 2
    Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0 /
    by Prabhu, Ramadas K.
    Published 2001
    Government Document Book
  3. 3
    Summary report of the orbital X-34 wing static aeroelastic study /
    by Prabhu, Ramadas K.
    Published 2001
    Government Document Book
  4. 4
    Inviscid flow computations of several aeroshell configurations for a '07 Mars lander /
    by Prabhu, Ramadas K.
    Published 2001
    Government Document Book
  5. 5
    Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24 /
    by Prabhu, Ramadas K.
    Published 2001
    Government Document Book
  6. 6
    An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5 /
    by Prabhu, Ramadas K.
    Published 2001
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    Government Document Microform Book
  7. 7
    Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees /
    by Prabhu, Ramadas K.
    Published 2001
    Get full text
    Government Document Microform Book
  8. 8
    Finite-rate water condensation in combustion-heated wind tunnels /
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    Government Document eBook
  9. 9
    Finite-rate water condensation in combustion-heated wind tunnels /
    by Erickson, Wayne D.
    Published 1988
    Other Authors: “...Prabhu, Ramadas K....”
    Get full text
    Government Document Book
  10. 10
    Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel /
    by Venkateswaran, S.
    Published 1992
    Other Authors: “...Prabhu, Ramadas K....”
    Government Document Book
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