Data, of interest to airplane designers, on flutter and vibration of structures to which control surfaces are attached; this source of danger may be controlled; modern methods of stress analyses and load factors in current use are adequate to provide all strength needed in airplane structures for flight in rough air, and for all necessary maneuvers. Before Int Automotive Eng Congress.


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    Titel :

    Airplane vibrations and flutter controllable by design


    Weitere Titelangaben:

    Soc Automotive Engrs J


    Beteiligte:
    Roche, J.A. (Autor:in)


    Erscheinungsdatum :

    1933


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




    Airplane Vibrations and Flutter Controllable by Design

    Roché, J. A. | SAE Technical Papers | 1933


    Airplane flutter demonstrated

    Engineering Index Backfile | 1929


    Flight flutter testing the B-58 airplane

    Mahaffey, P. T. | NTRS | 1975


    Airplane vibration tests as related to flutter problem

    Lyman, C.B. | Engineering Index Backfile | 1941


    Airplane vibration tests as related to flutter problem

    Lyman, C.B. | Engineering Index Backfile | 1941