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 Flight v 60 n 2229 Oct 12 1951 p 488-9)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Structural problems of future aircraft


    Additional title:

    Engineering


    Contributors:
    Hoff, N.J. (author)

    Published in:

    Engineering ; 172 , n 4475


    Publication date :

    1951


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Structural problems of future aircraft

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


    Aircraft fuelling problems of future

    Engineering Index Backfile | 1956


    Engineering problems of future aircraft

    Engineering Index Backfile | 1946


    Engineering problems of future aircraft

    Engineering Index Backfile | 1946