J.H. Argyris, S. Kelsey

The paper presents a summary and extension of the matrix force method of structural analysis given in Ref. [l]. The methods developed may be used on any structure but the report stresses particularly the aeronautical applications. The novel analysis of systems with cut-outs proposed in Ref. [l] is generalised here to include also structures of which some elements are modified (see also Ref. [2]). Thus, it is found possible to express the stresses in a modified system solely in terms of the stresses of the original system prior to modifications. The theory is illustrated on an example calculated on a digital computer and including the effects of a thermal loading case. The use of the digital computer is stressed throughout the report.

WGL-Tagung, Braunschweig, 1956

Conference Paper

englisch

21,0 x 29,7 cm, 21 Seiten

Jahrbuch der Wissenschaftlichen Gesellschaft für Luftfahrt, 1956; S.78-98; 1956; Braunschweig : Vieweg

NA

Bestellbar

1957