Deformation analysis of wing structures
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Author
Contributions
- United States. National Advisory Committee for Aeronautics - Contributor
- Langley Aeronautical Laboratory - Contributor
Publication
1947 - National Advisory Committee for Aeronautics, Washington, D.C, District of Columbia
Language
English
Word Count
8,500 words, Guess
Page Count
34 pages
Identifiers
- ISBN-101680156071
- ISBN-139781680156072
- OCLC Control Number919093439
- Open LibraryOL44477735M
Classifications
- LCCTA417.6
- DDC620.1123
Alternate Titles
- Technical Report Archive & Image Library (TRAIL)
Description
The elementary theories of bending and torsion often do not describe the stresses in aircraft shell structures with adequate accuracy; more refined stress theories have therefore have developed over a period of years. Theories of this nature are applied to the problem of calculating the deflections, particularly of wings. Bending as well as torsional deflections are discussed for wings without or with cut-outs. Whenever convenient, the formulas are given in such a form that they yield corrections to be added to the deflections calculated by means of the elementary theories. Examples show that the deflection corrections usually are quite small; very simple approximation formulas are therefore adequate for design purposes when conventional structures uder a reasonably uniform loading are being considered.
Subjects
Series Statement
- National Advisory Committee for Aeronautics technical note -- number 1361
- Technical note (United States. National Advisory Committee for Aeronautics) -- no. 1361.
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