Combination of greater speed and higher weight means that aircraft structure has been forced to absorb increasingly higher loads, yet aerodynamicist is constantly seeking thinner wings and slimmer bodies in which to place growing structural needs of modern high speed airplane; unequivocal point at which compromise will become necessary will be determined by fatigue strength of structure; solution to problem discussed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    High speed aircraft structure fatigue


    Weitere Titelangaben:

    Aero Digest


    Beteiligte:
    McLarren, R. (Autor:in)

    Erschienen in:

    Aero Digest ; 63 , n 3 ; p 100-108


    Erscheinungsdatum :

    1951


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Nonlinear Response and Sonic Fatigue of High Speed Aircraft

    Vaicaitis, R. / Kavallieratos, P. / Deutsche Gesellschaft fur Luft- und Raumfahrt e.V. et al. | British Library Conference Proceedings | 1992


    Thermal protection structure of high-speed aircraft

    WANG CHAO / XU RUINA / JIANG PEIXUE | Europäisches Patentamt | 2020

    Freier Zugriff

    High speed aircraft

    Clarkson, R.M. | Engineering Index Backfile | 1936


    High-speed Aircraft

    Schrenk, M | NTRS | 1934


    HIGH-SPEED AIRCRAFT

    NAZARENKO VADIM VADIMOVICH / BUDYKA SERGEJ MIKHAJLOVICH / DMITRIEVA ALEKSANDRA ANATOLEVNA et al. | Europäisches Patentamt | 2020

    Freier Zugriff