The strength and stiffness of shear webs with and without lightening holes
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Author
Contributions
- United States. National Advisory Committee for Aeronautics - Contributor
- Langley Aeronautical Laboratory - Contributor
Publication
1942 - National Advisory Committee for Aeronautics, Washington, D.C, District of Columbia
Language
English
Word Count
7,250 words, Guess
Page Count
29 pages
Identifiers
- ISBN-101680156535
- ISBN-139781680156539
- OCLC Control Number919163322
- Open LibraryOL44477787M
Classifications
- DDC620.186
- LCCTA480.A6
Alternate Titles
- NACA Wartime Reports. Series L.
Description
Nearly 200 tests were made on the strength of shear webs of 24S-T aluminum alloy, with and without lightening holes. The tests were made in a jig of the single-specimen type, in which the specimen is free to collapse completely without developing diagonal tension. The lightening holes were circular and had either flanged edges or beaded edges, the specimens with flanged edges constituting by far the largest test group.
Subjects
Series Statement
- Wartime Report / National Advisory Committee for Aeronautics -- number L402
- Wartime Reports (United States. National Advisory Committee for Aeronautics) -- no. L402.
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