Accession Number : AD0631397

Title :   STRUCTURAL ANALYSIS USING THE BALANCE METHOD.

Descriptive Note : Final rept.,

Corporate Author : ROME UNIV (ITALY) SCUOLA DI INGEGNERIA AERONAUTICA

Personal Author(s) : Broglio,Luigi

Report Date : DEC 1955

Pagination or Media Count : 27

Abstract : 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)

Descriptors :   (*AIRFRAMES, *STATICS), AERONAUTICS, AERODYNAMIC CONFIGURATIONS, LOAD DISTRIBUTION, MATHEMATICAL ANALYSIS, STRUCTURES

Subject Categories : Aircraft
      Structural Engineering and Building Technology

Distribution Statement : APPROVED FOR PUBLIC RELEASE