Showing 1 - 20 results of 140 for search '', query time: 0.15s 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
    Experimental study of saddle point of attachment in laminar juncture flow /
    by Coon, Michael D.
    Published 1995
    Government Document Book
  4. 4
    Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions /
    by Wood, William A.
    Published 1999
    Government Document Book
  5. 5
    Boundary layer transition in the leading edge region of a swept cylinder in high speed flow /
    by Coleman, Colin P.
    Published 1998
    Government Document Book
  6. 6
    Flight wing surface pressure and boundary-layer data report from the F-111 smooth variable-camber supercritical mission adaptive wing /
    by Powers, Sheryll Goecke
    Published 1997
    Government Document Book
  7. 7
    Measurements of heat transfer, flow, and pressures in a simulated turbine blade internal cooling passage /
    Published 1997
    Government Document Book
  8. 8
    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
  9. 9
    Effect of Reynolds number on the subsonic boattail drag of several wing-body configurations /
    by Reubush, David E.
    Published 1976
    Government Document Book
  10. 10
    High Reynolds number research : a workshop /
    Published 1977
    Government Document Conference Proceeding Book
  11. 11
    Static aerodynamic characteristics of a typical single-engine low-wing general aviation design for an angle-of-attack range of - 8 ̊to 90 ̊ /
    by Bihrle, William
    Published 1978
    Government Document Book
  12. 12
    Representation of turbulent shear stress by a product of mean velocity differences /
    by Braun, Willis H.
    Published 1977
    Government Document Book
  13. 13
    High Reynolds number research : a worksher /
    Published 1981
    Government Document Conference Proceeding Book
  14. 14
    Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 /
    by Noonan, Kevin W.
    Published 1980
    Government Document Book
  15. 15
    A hybridized method for computing high-reynolds-number hypersonic flow about blunt bodies /
    by Weilmuenster, K. James
    Published 1979
    Government Document Book
  16. 16
    Reynolds number tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel /
    by Jenkins, Renaldo V.
    Published 1983
    Government Document Book
  17. 17
    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
  18. 18
    High Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-meter transonic cryogenic tunnel /
    Published 1982
    Government Document Book
  19. 19
    The boundary layer on compressor cascade blades /
    by Deutsch, Steven
    Published 1984
    Government Document Book
  20. 20
    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
Search Tools: RSS Feed – Email Search