1–20 von 39 Ergebnissen
|

    Status report on NASA two-segment approach program

    Denery, D. G. / Bourquin, K. R. / Drinkwater, F. J., III et al. | NTRS | 1975

    Flight investigation of methods for implementing noise-abatement landing approaches

    Fry, E. B. / Innis, R. C. / Quigley, H. C. | NTRS | 1968

    Flight experience with the OGEE wing at low speed.

    Drinkwater, F. J., III / Rolls, L. S. | NTRS | 1965

    Pilot assessment aspects of simulation

    Cooper, G. E. / Drinkwater, F. J., III | NTRS | 1970

    Research pilots' observations of aircraft performance on a grooved runway

    Drinkwater, F. J., III / Patton, J. M., Jr. / Price, C. | NTRS | 1969

    New capabilities and recent research programs of the NASA/Army CH-47B variable-stability helicopter

    Hindson, W. S. / Hilbert, K. B. / Tucker, G. E. et al. | NTRS | 1986

    Technique for calculating optimum noise-abatement take-off profiles

    Drinkwater, F. J., III / Erzberger, H. / Lee, H. Q. et al. | NTRS | 1968

    Simulator investigations of various control systems for VTOL aircraft

    Fry, E. B. / Gerdes, R. M. / Gossett, T. D. et al. | NTRS | 1966

    The influence of motion on the effectiveness of flight simulators in training maneuvers

    Bray, R. S. / Drinkwater, F. J., III / Fry, E. B. | NTRS | 1971

    VTOL control system studies on a six-degree- of-freedom motion simulator

    Fry, E. B. / Gerdes, R. M. / Gossett, T. D. et al. | NTRS | 1966

    Low-lift-to-drag-ratio approach and landing studies using a CV-990 airplane

    Kock, B. M. / Fulton, F. L. / Drinkwater, F. J., III | NTRS | 1972

    Flight investigation of the aerodynamic properties of an Ogee wing

    Drinkwater, F. J., III / Koenig, D. G. / Rolls, L. S. | NTRS | 1965

    Use of very weak radiation sources to determine aircraft runway position

    Drinkwater, F. J., III / Kibort, B. R. | NTRS | 1965