The influence of impact velocity on the tensile characteristics of some aircraft metals and alloys
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Author
Contributions
- United States. National Advisory Committee for Aeronautics - Contributor
Publication
1942 - 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-101680156322
- ISBN-139781680156324
- OCLC Control Number914577145
- Open LibraryOL44477695M
Classifications
- DDC629.134
- LCCTL698
Description
This report deals principally with the results of tension tests on sixteen metals and alloys, most of which are employed extensively in aircraft construction. The tension characteristics are discussed for static conditions and rates of deformation up to about 150 feed per second. As a result of these tests, it has been shown that Dowmetal M and 18-percent chromium - 8 percent nickel stainless steel are adversely affected by an increasing rate of deformation. The other materials tested exhibit changes in yield stress, ultimate strength, and other tensile properties.
Series Statement
- Technical note / National Advisory Committee for Aeronautics -- no. 868
- Technical note (United States. National Advisory Committee for Aeronautics) -- 868.
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