An edition of Recommendations for numerical solution of reinforced-panel and fuselage-ring problems (1949)

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

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Recommendations for numerical solution of rei ...
Nicholas J. Hoff, Nicholas J. ...
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Last edited by MARC Bot
December 19, 2022 | History
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An edition of Recommendations for numerical solution of reinforced-panel and fuselage-ring problems (1949)

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

by

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 easily determined. The method of systematic relaxations, the matrix-calculus method, and several other methods applicable in special cases are discussed. Definite recommendations are made for obtaining the solution of reinforced-panel problems which are generally designated as shear lag problems. The procedures recommended are demonstrated in the analysis of a number of panels. In the case of fuselage rings it is not possible to make definite recommendations for the solution of the equilibrium equations for all rings and loadings. --

Publish Date
Publisher
U.S. Government Printing Office
Language
English
Pages
29

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Subjects

Aeronautics, Research, Airplanes, Fuselage, Design and construction, Aéronautique, Recherche, Avions, Conception et construction, Fuselages
Edition Availability
Cover of: Recommendations for numerical solution of reinforced-panel and fuselage-ring problems
Recommendations for numerical solution of reinforced-panel and fuselage-ring problems
1949, U.S. Government Printing Office
in English

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Book Details

Edition Notes

Includes bibliographical references (page 21).

Published in
Washington, D.C
Series
Report / National Advisory Committee for Aeronautics -- number 934, Report (United States. National Advisory Committee for Aeronautics) -- no. 934.

Classifications

Dewey Decimal Class
629.4
Library of Congress
TL501 .U52 1949eb

The Physical Object

Pagination
1 online resource (29 pages)
Number of pages
29

Edition Identifiers

Open Library
OL44477785M
ISBN 10
1680156462
ISBN 13
9781680156461
OCLC/WorldCat
919161696

Work Identifiers

Work ID
OL32663443W

Source records

marc_columbia MARC record

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December 19, 2022 Created by MARC Bot Imported from marc_columbia MARC record