Preliminary designs are developed for five V/STOL 10-ton cargo transports capable of 1800 nautical mi range; peak loads and stresses are calculated from structural dynamic response to ground handling, flight maneuver, gust penetration, and landing; loads and stresses are compared to those used to originally design aircraft; results are tabulated in matrix showing degree of relative criticalness for conditions investigated for each V/STOL configuration.


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    Titel :

    Structural dynamic response of large logistic V/STOL aircraft


    Weitere Titelangaben:

    Am Helicopter Soc -- J


    Beteiligte:
    Rich, M.J. (Autor:in) / Stebbins, R.F. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1967


    Format / Umfang :

    16 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    V/STOL aircraft structural considerations

    Alvey, V.W. / Fried, H. | Engineering Index Backfile | 1966


    V/STOL Aircraft Structural Considerations

    Fried, H. / Alvey, V. W. | SAE Technical Papers | 1966


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