Showing 1 - 20 results of 71 for search '', query time: 0.06s Refine Results
  1. 1
    Active control of instabilities in laminar boundary-layer flow

    Active control of instabilities in laminar boundary-layer flow by Joslin, Ronald D. (Ronald Douglas), 1963-

    Hampton, VA : [Springfield, Va.] : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


    Save to List
    Saved in:
  2. 2
    Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia : final report

    Experiments to verify nonparallel stability theory at Virginia Polytechnic Institute and State University, Blacksburg, Virginia : final report by Saric, W. S.

    Tempe, Ariz. : [Washington, DC] : [Springfield, Va.] : Dept. of Mechanical and Aerospace Engineering, Arizona State University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1988
    Format: Government Document Book


    Save to List
    Saved in:
  3. 3
    A quiet tunnel investigation of hypersonic boundary-layer stability over a cooled, flared cone : final report

    A quiet tunnel investigation of hypersonic boundary-layer stability over a cooled, flared cone : final report by Selby, Gregory V.

    Norfolk, Va. : [Washington, DC] : [Springfield, Va.] : Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


    Save to List
    Saved in:
  4. 4
    High Reynolds number hybrid laminar flow control (HLFC) flight experiment. II, Aerodynamic design

    High Reynolds number hybrid laminar flow control (HLFC) flight experiment. II, Aerodynamic design

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1999
    Format: Government Document Book


    Save to List
    Saved in:
  5. 5
    A concept for transition mapping on a 10°-cone in the National Transonic Facility using flow-pressure variation

    A concept for transition mapping on a 10°-cone in the National Transonic Facility using flow-pressure variation by Gartenberg, Ehud

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


    Save to List
    Saved in:
  6. 6
    Rapport d'essais du profil CAST 10 en transition dʹeclenchʹee, effectuʹes dans la soufflerie transsonique cryogʹenique T2 en pr'esence de parois auto-adaptables : Report on tests of a CAST 10 airfoil with fixed transition in the T2 transonic cryogenic wind tunnel with self-adaptive walls

    Rapport d'essais du profil CAST 10 en transition dʹeclenchʹee, effectuʹes dans la soufflerie transsonique cryogʹenique T2 en pr'esence de parois auto-adaptables : Report on tests o... by Seraudie, A.

    Toulouse : [Washington, DC] : [Springfield, Va.] : Centre DʹEtudes et de Recherches de Toulouse, Dept., DʹEtudes et de Recherches en Aerothermodynamique ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1985
    Format: Government Document Book


    Save to List
    Saved in:
  7. 7
    Instantaneous structure of turbulent separated boundary layers : report of research performed during the period August 3, 1995 to August 20, 1996, with support of grant number NAG 1 1530

    Instantaneous structure of turbulent separated boundary layers : report of research performed during the period August 3, 1995 to August 20, 1996, with support of grant number NAG... by Adrian, R. J. (Ronald J.)

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


    Save to List
    Saved in:
  8. 8
    Boundary layer transition in the leading edge region of a swept cylinder in high speed flow

    Boundary layer transition in the leading edge region of a swept cylinder in high speed flow by Coleman, Colin P.

    Moffett Field, Calif. : Springfield, VA : National Aeronautics and Space Administration, Ames Research Center ; National Technical Information Service, distributor, 1998
    Format: Government Document Book


    Save to List
    Saved in:
  9. 9
    Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment

    Boundary-layer transition results from the F-16XL-2 supersonic laminar flow control experiment by Marshall, Laurie A.

    Edwards, Calif. : Hanover, Md. : Springfield, Va. : National Aeronautics and Space Administration, Dryden Flight Research Center ; NASA Center for AeroSpace Information [distributor] ; National Technical Information Service [distributor], 1999
    Format: Government Document Book


    Save to List
    Saved in:
  10. 10
    Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate) : final report of TsAGI under cooperative agreement # NCCW-72.

    Receptivity of flat-plate boundary layer in a non-uniform free stream (vorticity normal to the plate) : final report of TsAGI under cooperative agreement # NCCW-72.

    Zhukovsky, Russia : [Washington, DC] : [Springfield, Va.] : Central Aero-Hydrodynamics Institute ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


    Save to List
    Saved in:
  11. 11
    An experimental investigation on location of boundary layer transition on the NACA 0012 using surface hot film gages

    An experimental investigation on location of boundary layer transition on the NACA 0012 using surface hot film gages by Wang, Tie-cheng

    Washington DC : National Aeronautics and Space Administration, 1986
    Format: Government Document Book


    Save to List
    Saved in:
  12. 12
    Analysis of the leading edge effects on the boundary layer transition : technical report, March 1, 1984 - August 31, 1990

    Analysis of the leading edge effects on the boundary layer transition : technical report, March 1, 1984 - August 31, 1990 by Chow, P. L. (Pao Liu), 1936-

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1990
    Format: Government Document Book


    Save to List
    Saved in:
  13. 13
    Swept-wing receptivity studies using distributed roughness : annual technical report

    Swept-wing receptivity studies using distributed roughness : annual technical report by Saric, W. S.

    Tempe, AZ : Hampton, Va. : [Springfield, Va.] : Mechanical and Aerospace Engineering, College of Engineering and Applied Science, Arizona State University ; National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1998
    Format: Government Document Book


    Save to List
    Saved in:
  14. 14
    A comparison of hypersonic vehicle flight and prediction results

    A comparison of hypersonic vehicle flight and prediction results by Iliff, Kenneth W.

    Edwards, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Dryden Flight Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


    Save to List
    Saved in:
  15. 15
    Annual progress report ... entitled "an experimental investigation of the flow physics of high-lift systems" for the period March-December 1995

    Annual progress report ... entitled "an experimental investigation of the flow physics of high-lift systems" for the period March-December 1995 by Thomas, Flint O.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


    Save to List
    Saved in:
  16. 16
    Distributed-roughness effects on stability and transition in swept-wing boundary layers : annual technical report ... NASA-Langley cooperative agreement # NCC-1-194 and the Boeing Company contract #ZA0078, during 5/17/96-12/31/96

    Distributed-roughness effects on stability and transition in swept-wing boundary layers : annual technical report ... NASA-Langley cooperative agreement # NCC-1-194 and the Boeing... by Carrillo, Ruben B.

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


    Save to List
    Saved in:
  17. 17
    Laser transit anemometer measurements on a slender cone in the Langley unitary plan wind tunnel

    Laser transit anemometer measurements on a slender cone in the Langley unitary plan wind tunnel

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1990
    Format: Government Document Book


    Save to List
    Saved in:
  18. 18
    The role of nonlinear critical layers in boundary layer transition

    The role of nonlinear critical layers in boundary layer transition by Goldstein, M. E.

    [Washington, D.C.] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


    Save to List
    Saved in:
  19. 19
    Some characteristics of bypass transition in a heated boundary layer

    Some characteristics of bypass transition in a heated boundary layer by Sohn, K. H.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration ; [National Technical Information Service, distributor], 1989
    Format: Government Document Book


    Save to List
    Saved in:
  20. 20
    Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle : final report

    Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle : final report by Wolf, Stephen W. D.

    San Jose, Calif. : [Washington, D.C.] : [Springfield, Va.] : MCAT Institute ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


    Save to List
    Saved in:

Search Tools: