Showing 1 - 20 results of 33 for search '', query time: 0.21s Refine Results
  1. 1
    Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges /
    by Chu, Julio
    Published 1996
    Government Document Book
  2. 2
    Research and applications in aeroelasticity and structural dynamics at the NASA Langley Research Center /
    by Abel, Irving
    Published 1997
    Government Document Book
  3. 3
    Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions /
    by Wood, William A.
    Published 1999
    Government Document Book
  4. 4
    Experimental investigation to validate use of cryogenic temperatures to achieve high Reynolds numbers in boattail pressure testing /
    by Reubush, David E.
    Published 1976
    Government Document Book
  5. 5
    Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations /
    by Reubush, David E.
    Published 1976
    Government Document Book
  6. 6
    A hybridized method for computing high-reynolds-number hypersonic flow about blunt bodies /
    by Weilmuenster, K. James
    Published 1979
    Government Document Book
  7. 7
    A review of some Reynolds number effects related to bodies at high angles of attack /
    by Polhamus, Edward C., 1948-
    Published 1984
    Government Document Book
  8. 8
    High Reynolds number tests of the cast 10-2/DOA 2 airfoil in the Langley 0.3-meter transonic cryogenic tunnel - phase II /
    Published 1984
    Government Document Book
  9. 9
    Highlights of unsteady pressure tests on a 14 percent supercritical airfoil at high Reynolds number, transonic condition /
    Published 1987
    Government Document Book
  10. 10
    A finite Reynolds number approach for the prediction of boundary layer receptivity in localized regions /
    by Choudhari, Meelan
    Published 1991
    Government Document Book
  11. 11
    Reynolds number influences in aeronautics /
    Published 1993
    Government Document Book
  12. 12
    Wing pressure distributions from subsonic tests of a high-wing transport model.
    by Applin, Zachary T.
    Published 1995
    Government Document Book
  13. 13
    Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers.
    by Choudhari, Meelan
    Published 1995
    Government Document Book
  14. 14
    Assessment of dual-point drag reduction for an executive-jet modified airfoil section /
    by Allison, Dennis O.
    Published 1996
    Government Document Book
  15. 15
    Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions /
    by Bartels, Robert E.
    Published 1997
    Government Document Book
  16. 16
    Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing /
    Published 1997
    Government Document Book
  17. 17
    Results of aerothermodynamic and boundary layer transition testing of 0.0362-Scale X-38 (Rev 3.1) vehicle in NASA Langley 20-inch Mach 6 tunnel /
    Published 1997
    Government Document Book
  18. 18
    Overview of HATP experimental aerodynamics data for the baseline F/A-18 configuration : High-Angle-of-Attack Technology Conference /
    Published 1996
    Government Document Book
  19. 19
    Navier-Stokes simulation of several high-lift reference H configurations /
    by Lessard, Wendy B.
    Published 1999
    Government Document Book
  20. 20
    Reynolds number effects on the performance of lateral control devices /
    by Mineck, Raymond E.
    Published 2000
    Government Document Book
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