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Displaying 1-11 of 11 results for author "Prabhu, Ramadas K."
An inviscid computational study of an X-33 configuration at hypersonic speeds [microform] / Ramadas K. Prabhu.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
Studies on the interference of wings and propeller slipstreams [microform] : final report for the period ending December 31, 1984 / by Ramadas K. Prabhu and Surendra N. Tiwari, principal investigator.
- Text
- Norfolk, Va. : Old Dominion University Research Foundation ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1985]
- 1985
An implementation of a chemical and thermal nonequilibrium flow solver on unstructured meshes and application to blunt bodies [microform] / Ramadas K. Prabhu.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1994]
- 1994
An approximate Riemann solver for thermal and chemical nonequilibrium flows [microform] / Ramadas K. Prabhu.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis [microform] / Ramadas K. Prabhu.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Inviscid flow computations of several aeroshell configurations for a '07 Mars lander [microform] / Ramadas K. Prabhu ; prepared for ... under contract NAS1-96014.
- Text
- Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
- 2001
Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24 [microform] / Ramadas K. Prabhu ; [prepared ... under contract NAS1-00135].
- Text
- Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
- 2001
Summary report of the orbital X-34 wing static aeroelastic study [microform] / Ramadas K. Prabhu ; prepared ... under contract NAS1-96014.
- Text
- Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
- 2001
Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0 [microform] / Ramadas K. Prabhu ; [prepared ... under contract NAS1-96014].
- Text
- Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
- 2001
Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees [microform] / Ramadas K. Prabhu.
- Text
- Hampton, Va. : National Aeronautics and Science Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information, [2001]
- 2001
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS39080An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5 [microform] / Ramadas K. Prabhu.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2001]
- 2001
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS39078
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