1–7 von 7 Ergebnissen
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    Effects of atmosphere and aircraft motion on location and intensity of sonic boom

    Friedman, M.P. / Kane, E.J. / Sigalla, A. | Engineering Index Backfile | 1963
    traveled; application of theory is made in considering sonic boom caused by supersonic aircraft; problems such as complete acoustic refraction and ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA)

    Unsteady aerodynamic forces on slender supersonic aircraft with flexible wings and bodies

    Yates, J.E. / Zeydel, E.F.E. | Engineering Index Backfile | 1963
    Paper derives generalized aerodynamic forces for aircraft on basis of slender body theory; configurations are considered which are spanwise ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA)

    Decay of trailing vortices

    Sherries, H.E. | Engineering Index Backfile | 1968
    Decay of trailing vortices was experimentally studied and parameters affecting decay rate related to flight conditions and basic aircraft ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA)

    Analysis of helicopter aeroelastic characteristics in high-speed flight

    Gerstenberger, W. / Wood, E.R. | Engineering Index Backfile | 1963
    Analytical method, which can be used for performance, stress, and vibration studies of helicopters and VTOL aircraft; applications are ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA)

    Jet flap characteristics for high-aspect-ratio wings

    Korbacher, G.K. | Engineering Index Backfile | 1964
    Thrust hypothesis, concept and experimental verification; "characteristics" for jet-flapped wings at zero and nonzero angle of attack are ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA)

    Time-optimal flight paths

    Berry, R.L. | Engineering Index Backfile | 1968
    drag laws were used; model aircraft was assumed to have turbojet propulsion system; it was found that form of thrust and drag laws does not ...
    Verlag: American Institute of Aeronautics and Astronautics (AIAA)

    Water-augmented turbofan engine

    Davison, W.R. / Sadowski, T.J. | Engineering Index Backfile | 1968
    discharge duct of aircraft-type turbofan engine; theoretical design and off-design performance show that dry thrust theoretically can be augmented ...