Stress and distortion measurements in a 45 degree swept box beam subjected to bending and to torsion
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Author
Contributions
- Libove, Charles - Contributor
- United States. National Advisory Committee for Aeronautics - Contributor
Publication
1948 - National Advisory Committee for Aeronautics, Washington, D.C, District of Columbia
Language
English
Word Count
9,500 words, Guess
Page Count
38 pages
Identifiers
- ISBN-101680156136
- ISBN-139781680156133
- OCLC Control Number919094329
- Open LibraryOL44477747M
Classifications
- DDC624.17723
- LCCTA660.B4
Alternate Titles
- Technical Report Archive & Image Library (TRAIL)
Description
An untapered aluminum-alloy box beam, representing the main structural component of a full-span, two-spar, 45 degree swept wing with a carry-through bay, was subjected to tip bending and twisting loads and its stresses and distortions were meaured. Only symmetrical loading was considered and the stresses were kept below the proportional limit.
Subjects
Topics
Series Statement
- National Advisory Committee for Aeronautics technical note -- number 1525
- Technical note (United States. National Advisory Committee for Aeronautics) -- no. 1525.
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