Showing 1 - 20 results of 40 for search '', query time: 0.45s Refine Results
  1. 1
    Thermal analysis of a metallic wing glove for a Mach-8 boundary-layer experiment /
    by Gong, Leslie
    Published 1998
    Government Document Book
  2. 2
    Finite-element analysis of a Mach-8 flight test article using nonlinear contact elements /
    by Richards, W. Lance
    Published 1997
    Government Document Book
  3. 3
    Recent flight test results of the joint CIAM-NASA Mach 6.5 Scramjet Flight Program /
    by Roudakov, Alexander S.
    Published 1998
    Government Document Book
  4. 4
    Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept /
    by Hahne, David E.
    Published 1997
    Government Document Book
  5. 5
    The NASA Hyper-X Program /
    Published 1997
    Government Document Book
  6. 6
    Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10.
    by Holland, Scott D.
    Published 1995
    Government Document Book
  7. 7
    Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code.
    by Kapoor, Kamlesh
    Published 1994
    Government Document Book
  8. 8
    Mach 10 computational study of a three-dimensional scramjet inlet flow field.
    by Holland, Scott D.
    Published 1995
    Government Document Book
  9. 9
    Performance of an aerodynamic yaw controller mounted on the space shuttle orbiter body flap at Mach 10.
    by Scallion, W. I.
    Published 1995
    Government Document Book
  10. 10
    A fully implicit time accurate method for hypersonic combustion : application to shock-induced combustion instability.
    by Yungster, Shaye
    Published 1994
    Government Document Book
  11. 11
    Mach 5 to 7 RBCC propulsion system testing at NASA-LeRC HTF /
    by Perkins, H. Douglas
    Published 1996
    Government Document Book
  12. 12
    Effect of fin leading edge sweep on shock-shock interaction at Mach 6 /
    by Berry, Scott A.
    Published 1996
    Government Document Book
  13. 13
    Real-time method for estimating viscous forebody drag coefficients /
    Published 2000
    Government Document Book
  14. 14
    Multiphysics simulation of active hypersonic lip cooling /
    by Melis, Matthew E.
    Published 1999
    Government Document Book
  15. 15
    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
  16. 16
    Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system /
    by DeBonis, J. R.
    Published 2001
    Adobe Acrobat Reader required
    Government Document Book
  17. 17
    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
  18. 18
    Mach 6 flow field surveys beneath the forebody of an airbreathing missile /
    by Johnston, Patrick J.
    Published 1986
    Government Document Book
  19. 19
    Mach 10 experimental database of a three-dimensional scramjet inlet flow field /
    by Holland, Scott D.
    Published 1995
    Get full text
    Government Document Book
  20. 20
    On the instability of hypersonic flow past a flat plate /
    by Blackaby, Nicholas
    Published 1990
    Get full text
    Government Document Book
Search Tools: RSS Feed – Email Search