A DSIR Sponsored Research Programme on the Development and Application of the Matrix Force Method and the Digital Computer. The present issue gives a summary of the basic theory of the matrix force method together with some necessary extensions for the fuselage problem. The equilibrium conditions for the idealized structure are then examined in detail and the relevant equations of equilibrium established in matrix form.


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    Title :

    The Analysis of Fuselages of Arbitrary Cross-section and Taper


    Contributors:
    Argyris, J.H. (author) / Kelsey, S. (author)

    Published in:

    Publication date :

    1959-04-01


    Size :

    12 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    The Analysis of Fuselages of Arbitrary Cross-section and Taper

    Argyris, J.H. / Kelsey, S. | Emerald Group Publishing | 1959


    The Analysis of Fuselages of Arbitrary Cross-section and Taper

    Argyris, J.H. / Kelsey, S. | Emerald Group Publishing | 1961


    The Analysis of Fuselages of Arbitrary Cross-section and Taper

    Argyris, J.H. / Kelsey, S. | Emerald Group Publishing | 1959


    The Analysis of Fuselages of Arbitrary Cross-section and Taper

    Argyris, J.H. / Kelsey, S. | Emerald Group Publishing | 1961


    The Analysis of Fuselages of Arbitrary Cross-section and Taper

    Argyris, J.H. / Kelsey, S. | Emerald Group Publishing | 1959