The paper describes an approximate method for the direct stress analysis of anisotropic swept cantilever plates, without the usual need for intermediate deflection calculations. The method of analysis employs the Principle of Least Work, in conjunction with the assumption that the load and stress components may be represented with sufficient accuracy by a power series in the chordwise co-ordinate, the coefficients of this series being functions of the spanwise position only. The validity is thus limited to these loadings for which the series involved are convergent. A system of oblique co-ordinates is used to simplify the analysis. Particular attention is focused on the parallelogram cantilever plate, subjected to a uniform normal loading and to a system of tip bending moments, twisting moments and shear forces. Theoretical predictions are compared with the results of an experimental investigation.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    The Direct Stress Anal/sis of Swept Cantilever Plates of Low Aspect Ratio


    Subtitle :

    An Approximate Method, employing the Principle of Least Work, which Obviates the Need for Intermediate Deflection Calculations


    Contributors:
    Coull, A. (author)

    Published in:

    Publication date :

    1965-06-01


    Size :

    9 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Bending of swept cantilever thin elastic plates.

    BASAVA RAJU / B. / SHAH, C. G. | AIAA | 1969


    EFFECT OF ASPECT RATIO ON SWEPT WING DYNAMIC STALL

    Hammer, Patrick R. / Garmann, Daniel J. / Visbal, Miguel R. | TIBKAT | 2021


    Effect of Aspect Ratio on Swept-Wing Dynamic Stall

    Hammer, Patrick R. / Garmann, Daniel J. / Visbal, Miguel R. | AIAA | 2023


    Effect of Aspect Ratio on Swept Wing Dynamic Stall

    Hammer, Patrick R. / Garmann, Daniel J. / Visbal, Miguel R. | AIAA | 2021


    Study of Low-Aspect Ratio Swept and Oblique Wings

    Edward J. Hopkins / Alan D. Levin | AIAA | 1975