Recommendations for numerical solution of reinforced-panel and fuselage-ring problems

Procedures are recommended for solving the equations of equilibrium of reinforced panels and isolated fuselage rings as represented by the external loads and the operations table established according to Southwell's method. From the solution of these equations the stress distribution can be eas...

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Bibliographic Details
Main Authors Hoff, Nicholas J. 1906- (Author), Libby, Paul A. (Author)
Corporate Authors United States. National Advisory Committee for Aeronautics, Polytechnic Institute of Brooklyn
Format Electronic eBook
LanguageEnglish
Published Washington, D.C. : U.S. Government Printing Office, 1949.
SeriesReport (United States. National Advisory Committee for Aeronautics) ; no. 934.
Subjects
Online AccessFull text
ISBN9781680156461
1680156462
Physical Description1 online resource (29 pages)

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