Structural difference between subsonic and supersonic wings; it is suggested that future aircraft be classified, from safety standpoint, in three categories; nonexpendable, semiexpendable and expendable; distinction attains great importance at Mach numbers above 2.0, because of effect of aerodynamic heating upon metals; phenomenon of creep necessitates introduction of semiexpendable class for piloted aircraft. Before 3rd Anglo-American Aeronautical Conference. (See also Engineering v 172 n 4475 Nov 2 1951 p 573-5)


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    Titel :

    Structural problems of future aircraft


    Weitere Titelangaben:

    Flight


    Beteiligte:
    Hoff, N.J. (Autor:in)

    Erschienen in:

    Flight ; 60 , n 2229


    Erscheinungsdatum :

    1951


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Structural problems of future aircraft

    Hoff, N.J. | Engineering Index Backfile | 1951


    Engineering problems of future aircraft

    Engineering Index Backfile | 1946


    Engineering problems of future aircraft

    Engineering Index Backfile | 1946


    Aircraft fuelling problems of future

    Engineering Index Backfile | 1956


    Problems in aircraft structural research

    Shanley, F.R. | Engineering Index Backfile | 1943