Showing 1 - 20 results of 43 for search '', query time: 0.21s Refine Results
  1. 1
    A Preliminary investigation of the use of throttles for emergency flight control /
    Published 1991
    Government Document Book
  2. 2
    Wind tunnel investigation of the interaction and breakdown characteristics of slender-wing vortices at subsonic, transonic, and supersonic speeds /
    by Erickson, Gary E.
    Published 1991
    Government Document Book
  3. 3
    Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2 /
    by Bare, E. Ann
    Published 1992
    Government Document Book
  4. 4
    Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds /
    by Wood, Richard M.
    Published 1992
    Government Document Book
  5. 5
    Feasibility of using a knowledge-based system concept for in-flight primary flight display research /
    by Ricks, Wendell R.
    Published 1991
    Government Document Book
  6. 6
    Static performance of a cruciform nozzle with multiaxis thrust-vectoring and reverse-thrust capabilities /
    by Wing, David J.
    Published 1992
    Government Document Book
  7. 7
    The natural flow wing-design concept /
    by Wood, Richard M.
    Published 1992
    Government Document Book
  8. 8
    Installation effects of wing-mounted turbofan nacelle-pylons on a 1/17-scale, twin-engine, low-wing transport model /
    Published 1992
    Government Document Book
  9. 9
    Flight-determined benefits of integrated flight-propulsion control systems /
    by Stewart, James F.
    Published 1992
    Government Document Book
  10. 10
    Integrated flight propulsion control research results using the NASA F-15 HIDEC flight research facility /
    by Stewart, James F.
    Published 1992
    Government Document Book
  11. 11
    Aircraft ground test and subscale model results of axial thrust loss caused by thrust vectoring using turning vanes /
    by Johnson, Steven A.
    Published 1992
    Government Document Book
  12. 12
    Design and experimental validation of a flutter suppression controller for the active flexible wing /
    by Waszak, Martin R.
    Published 1992
    Government Document Book
  13. 13
    Subsonic flight test evaluation of a performance seeking control algorithm on an F-15 airplane /
    by Gilyard, Glenn B.
    Published 1992
    Government Document Book
  14. 14
    Flight test results from a supercritical mission adaptive wing with smooth variable camber /
    Published 1992
    Government Document Book
  15. 15
    Correlation of forebody pressures and aircraft yawing moments on the X-29A aircraft at high angles of attack /
    by Fisher, David F.
    Published 1992
    Government Document Book
  16. 16
    Subsonic flight test evaluation of a propulsion system parameter estimation process for the F-10 engine /
    by Orme, John S.
    Published 1992
    Government Document Book
  17. 17
    In-flight flow visualization results from the X-29A aircraft at high angles of attack /
    by Del Frate, John H.
    Published 1992
    Government Document Book
  18. 18
    Pressure distribution for the wing of the YAV-8B airplane; with and without pylons /
    Published 1993
    Government Document Book
  19. 19
    Aerothermodynamic flow phenomena of the airframe-integrated supersonic combustion ramjet /
    by Walton, James T.
    Published 1992
    Government Document Book
  20. 20
    Effect of crash pulse shape on seat stroke requirements for limiting loads on occupants of aircraft /
    by Carden, Huey D.
    Published 1992
    Government Document Book
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