BEFORE a detailed consideration of internal stresses may be made, it is necessary to define external loadings which are possibly critical. This involves the consideration of manoeuvres throughout the altitude range of the aeroplane, to a severity fixed by aerodynamic or specification values of speed and normal acceleration.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Practical Structural Design Problems of Supersonic Aircraft


    Beteiligte:
    Heath, W.G. (Autor:in) / Heath, B.O. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1957-07-01


    Format / Umfang :

    10 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Practical structural design problems of supersonic aircraft

    Heath, W.G. / Heath, B.O. | Engineering Index Backfile | 1957


    Unique structural problems in supersonic aircraft design

    Michell, F.P. | Engineering Index Backfile | 1956


    Structural problems of supersonic aircraft

    van der Neut, A. | Engineering Index Backfile | 1960


    Supersonic-aircraft design

    Hunn, B.A. | Engineering Index Backfile | 1953


    SUPERSONIC AND TRANSONIC AIRCRAFT PROBLEMS

    REICHERT, CARL E. | SAE Technical Papers | 1950