STRUCTURAL ANALYSIS USING THE BALANCE METHOD.
ROME UNIV (ITALY) SCUOLA DI INGEGNERIA AERONAUTICA
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The work is divided in three parts Part 1 deals with the general rules of Balance--Method B.M., which is a general method of solution of problems of Mathematical Physics, originated by the Author part 2 deals with the B.M. application to advanced aeronautical structures multistringers shells, stressed--skin wings, etc. and part 3 deals with the application of B.M. to the swept wing problem. For this latest problem, it was, before all, necessary, to develop an adequate theory. The equations given by such theory were then integrated by using the B.M. For each of the above parts, a Technical Report was prepared. The three Technical Reports are summarized in this paper. Author
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