This paper develops general purpose programmes for an electronic digital computer for use when the Argyris Matrix Method of Structural Analysis is employed. Programmes for both the force and displacement methods are given and they apply for arbitrarily large structures. The procedure to be followed in the particular case of the structural analysis of a delta wing is outlined and the advantages of using magnetic tape storage are considered.
Aircraft Engineering and Aerospace Technology – Emerald Publishing
Published: May 1, 1956
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