Study made of rocking on curved fuselage under surface, following impact of tail or nose, to convert vertical energy in landing into energy of pitching oscillation in which wing lift changes and aerodynamic damping are important; computations of load and motions for given shapes and load applications for selected aircraft; analysis and experiment indicate that loads and moments are acceptable.


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    Titel :

    Skid landings of airplanes on rocker-type fuselages


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Mayo, W.L. (Autor:in)


    Erscheinungsdatum :

    1961


    Format / Umfang :

    61 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Theoretical stability analysis of skid-rocker landings of space vehicles

    Fralich, Robert W. / Kruszewski, Edwin T. | TIBKAT | 1963


    Multi-engine airplanes and forced landings

    Smith, H.G. | Engineering Index Backfile | 1926


    AIRCRAFT FUSELAGES

    DETERT BRUCE RAYMOND | Europäisches Patentamt | 2016

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