Showing 1 - 20 results of 28 for search '', query time: 0.07s Refine Results
  1. 1
    Improving CPA-TSD steady pressure solutions through airfoil slope modification

    Improving CPA-TSD steady pressure solutions through airfoil slope modification

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


    Save to List
    Saved in:
  2. 2
    Aerodynamics of heat exchangers for high-altitude aircraft

    Aerodynamics of heat exchangers for high-altitude aircraft by Drela, Mark

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


    Save to List
    Saved in:
  3. 3
    Wake geometry measurements and analytical calculations on a small-scale rotor model

    Wake geometry measurements and analytical calculations on a small-scale rotor model

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


    Save to List
    Saved in:
  4. 4
    In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)

    In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft) by Saltzman, Edwin J.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


    Save to List
    Saved in:
  5. 5
    A two dimensional study of rotor/airfoil interaction in hover

    A two dimensional study of rotor/airfoil interaction in hover by Lee, Chyang Sheng

    Moffett Field, Calif. : [Palo Alto, Calif.] : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center ; Stanford University ; [National Technical Information Service, distributor], 1988
    Format: Government Document Book


    Save to List
    Saved in:
  6. 6
    Development and testing of airfoils for high-altitude aircraft : final report

    Development and testing of airfoils for high-altitude aircraft : final report by Drela, Mark

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


    Save to List
    Saved in:
  7. 7
    Adaptive grid embedding for the two-dimensional flux-split Euler equations

    Adaptive grid embedding for the two-dimensional flux-split Euler equations by Warren, Gary Patrick

    Mississippi State, Miss. :; Mississippi State, Miss. : Mississippi State University, Dept. of Aerospace Engineering, 1990
    Format: Government Document Book


    Save to List
    Saved in:
  8. 8
    Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data : final report

    Viscous-flow analysis of a subsonic transport aircraft high-lift system and correlation with flight data : final report by Potter, R. C. (Richard Charles), 1936-

    Davis, Calif. : [Washington, DC] : [Springfield, Va.] : Dept. of Mechanical and Aeronautical Engineering, University of California ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


    Save to List
    Saved in:
  9. 9
    Effect of acoustic excitation on stalled flows over an airfoil

    Effect of acoustic excitation on stalled flows over an airfoil by Zaman, K. B. M. Q.

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


    Save to List
    Saved in:
  10. 10
    PROFILE : airfoil geometry manipulation and display : user's guide

    PROFILE : airfoil geometry manipulation and display : user's guide by Collins, Leslie

    Moffett Field, Calif. : [Springfield, Va.] : National Aeronautics and Space Administration, Ames Research Center ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


    Save to List
    Saved in:
  11. 11
    Determination of the pressure drag of airfoils by integration of surface pressures

    Determination of the pressure drag of airfoils by integration of surface pressures by Phillips, William H.

    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:
  12. 12
    Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations

    Computational test cases for a clipped delta wing with pitching and trailing-edge control surface oscillations by Bennett, Robert M. (Robert Merrill), 1945-

    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:
  13. 13
    Assessment of dual-point drag reduction for an executive-jet modified airfoil section

    Assessment of dual-point drag reduction for an executive-jet modified airfoil section by Allison, Dennis O.

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1996
    Format: Government Document Book


    Save to List
    Saved in:
  14. 14
    Application of a third order upwind scheme to viscous flow over clean and iced wings : 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV

    Application of a third order upwind scheme to viscous flow over clean and iced wings : 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV by Bangalore, A.

    Washington, D.C. : [Springfield, Va.] : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


    Save to List
    Saved in:
  15. 15
    Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes

    Temporal-adaptive Euler/Navier-Stokes algorithm for unsteady aerodynamic analysis of airfoils using unstructured dynamic meshes by Kleb, William L.

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


    Save to List
    Saved in:
  16. 16
    A feasibility study to control airfoil shape using THUNDER

    A feasibility study to control airfoil shape using THUNDER by Pinkerton, Jennifer L.

    Hampton, Va. : [Springfield, Va.] :; Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1997
    Format: Government Document Book


    Save to List
    Saved in:
  17. 17
    Numerical study to assess sulfur hexafluoride as a medium for testing multielement airfoils

    Numerical study to assess sulfur hexafluoride as a medium for testing multielement airfoils by Bonhaus, Daryl L.

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


    Save to List
    Saved in:
  18. 18
    Control theory based airfoil design for potential flow and a finite volume discretization

    Control theory based airfoil design for potential flow and a finite volume discretization by Reuther, James

    [Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], 1994
    Format: Government Document Book


    Save to List
    Saved in:
  19. 19
    Pressure distributions from subsonic tests of a NACA 0012 semispan wing model

    Pressure distributions from subsonic tests of a NACA 0012 semispan wing model by Applin, Zachary T.

    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:
  20. 20
    The development of a tool for semi-automated generation of structured and unstructured grids about isolated rotorcraft blades

    The development of a tool for semi-automated generation of structured and unstructured grids about isolated rotorcraft blades by Shanmugasundaram, Ramakrishnan

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


    Save to List
    Saved in:

Search Tools: