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  1. 1
    Low-speed wind-tunnel investigation of the effect of strakes and nose chines on lateral-directional stability of a fighter configuration /
    by Brandon, Jay M
    Published 1986

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  2. 2
    Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data
    by Klein, Vladislav
    Published 1998

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  3. 3
    Moving base simulation of an ASTOVL Lift-fan aircraft
    by Chung, William W. Y
    Published 1995

    Government Document Book
  4. 4
    Closed-loop system identification experience for flight control law and flying qualities evaluation of a high performance fighter aircraft
    by Murphy, Patrick C
    Published 1996

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  5. 5
    Euler technology assessment for preliminary aircraft design unstructured/structured grid NASTD application for aerodynamic analysis of an advanced fighter/tailless configuration /
    by Michal, Todd R
    Published 1998

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  6. 6
    Revised simulation model of the control system, displays, and propulsion system for an ASTOVL lift fan aircraft
    by Franklin, James A
    Published 1997

    Government Document Book
  7. 7
    Utilization of an agility assessment module in analysis and optimization of preliminary fighter configuration
    by Ngan, Angelen
    Published 1996

    Government Document Book
  8. 8
    An assessment of viscous effects in computational simulation of benign and burst vortex flows on generic fighter wind-tunnel models using TEAM code
    by Kinard, Tim A
    Published 1995

    Government Document Book
  9. 9
    Performance study for inlet installations
    by Bingaman, D. C
    Published 1992

    Government Document Book
  10. 10
    Aerodynamics of the Viggen 37 aircraft
    by Karling, Krister
    Published 1986

    Government Document Book
  11. 11
    Effect of emerging technology on a convertible, business/interceptor, supersonic-cruise jet /
    Published 1986

    Government Document Book
  12. 12
    Vortex flap technology a stability and control assessment /
    by Carey, K. M
    Published 1987

    Government Document Book
  13. 13
    Investigation into the impact of agility in conceptual fighter design
    by Engelbeck, R. M
    Published 1995

    Government Document Book
  14. 14
    Integrated helmet mounted display concepts for air combat
    by Clark, Joseph W
    Published 1995

    Government Document Book
  15. 15
    Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47 /

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  16. 16
    Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models
    by Charlton, Eric F
    Published 1998

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  17. 17
    Robust, decoupled, flight control design with rate saturated actuators
    by Snell, S. A
    Published 1997

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  18. 18
    Euler technology assessment SPLITFLOW code applications for stability and control analysis on an advanced fighter model employing innovative control concepts /
    by Jordan, Keith J
    Published 1998

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  19. 19
    Feasibility and benefits of laminar flow control on supersonic cruise airplanes
    by Powell, A. G
    Published 1989

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  20. 20
    Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept /
    by Riley, Donald R, Riley, Donald R
    Published 1989

    Government Document Book
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