1–20 von 97 Ergebnissen
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    Fixed base simulator study of an externally blown flap STOL transport airplane during approach and landing

    Grantham, W. D. / Nguyen, L. T. / Patton, J. M., Jr. et al. | NTRS | 1972

    Recent research related to prediction of stall/spin characteristics of fighter aircraft

    Nguyen, L. T. / Anglin, E. L. / Gilbert, W. P. | NTRS | 1976

    Aerodynamic characteristics in ground proximity

    Thomas, J. L. / Hassell, J. L., Jr. / Nguyen, L. T. | NTRS | 1976

    Use of piloted simulation for studies of fighter departure/spin susceptibility

    Gilbert, W. P. / Nguyen, L. T. | NTRS | 1978

    Results of piloted simulator studies of fighter aircraft at high angles of attack

    Chambers, J. R. / Gilbert, W. R. / Nguyen, L. T. | NTRS | 1978

    Control considerations for CCV fighters at high angles of attack

    Nguyen, L. T. / Gilbert, W. P. / Grafton, S. B. | NTRS | 1979

      Control considerations for CCV fighters at high angles of attack

      Nguyen, L. T. / Gibert, W. P. / Grafton, S. B. | NTRS | 1979

    Control-System Techniques for Improved Departure/Spin Resistance for Fighter Aircraft

    Luat T Nguyen / William P Gilbert / Marilyn E Ogburn | NTRS | 1980

    Application of high-alpha control system concepts to a variable-sweep fighter airplane

    Nguyen, L. T. / Gilbert, W. P. / Gera, J. et al. | NTRS | 1980

    Self-induced wing rock of slender delta wings

    Nguyen, L. T. / Yip, L. P. / Chambers, J. R. | NTRS | 1981

    Flight test experience with high-alpha control system techniques on the F-14 airplane

    Gera, J. / Wilson, R. J. / Enevoldson, E. K. et al. | NTRS | 1981

    High angle-of-attack characteristics of three-surface fighter aircraft

    Croom, M. A. / Grafton, S. B. / Nguyen, L. T. | NTRS | 1982