Examples of structures include conventional sheet-stringer panels, honeycomb panels, integrally machined and stiffened panels, trusscore panels and others; separate Zee stiffeners attached to thin skin are fabricated at low cost and have reasonable efficiencies; integrally machined and honeycomb panels are more efficient, and also are more expensive to fabricate; therefore, aerospace engineer is constantly seeking means of obtaining improved panel concepts that result in higher structural efficiency at lower manufacturing costs.


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    Titel :

    Comparison of integrally formed compression panel efficiencies with other aerospace panel concepts


    Weitere Titelangaben:

    AIAA-ASME Structures, Structural Dynamics Matls Conference


    Beteiligte:
    McClaren, S.W. (Autor:in) / McQueen, J.C. (Autor:in) / Martin, A.P. (Autor:in)

    Kongress:

    8th AIAA-ASME Structures, Structural Dynamics and Materials Conference ; 1967 Stresses



    Erscheinungsdatum :

    1967


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



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