Flat sheet metal girder with very thin metal web
Part 3 : Sheet metal girders with spars resistant to bending - the stress in uprights - diagonal tension fields
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Author
Contributions
- United States. National Advisory Committee for Aeronautics - Contributor
Publication
1931 - National Advisory Committee for Aeronautics, Washington, D.C, District of Columbia
Language
English
Word Count
9,750 words, Guess
Page Count
39 pages
Identifiers
- ISBN-101680156586
- ISBN-139781680156584
- OCLC Control Number914554301
- Open LibraryOL44477688M
Classifications
- DDC620.166
- LCCTA460
Description
This report continues the work presented in NACA-TM 605 and expands the scope to include the change in specific number of wrinkles from direction x to z, so that b and f become variable in direction z. Moreover, it seems likely that b and f increase from the edge toward the center if the sheet is infinitely thin.
Subjects
Series Statement
- Technical memorandums / National Advisory Committee for Aeronautics -- 606
- Technical memorandums (United States. National Committee for Aeronautics) -- no. 606.
Other Editions
- Flat sheet metal girder with very thin metal web: Part 3 : Sheet metal girders with spars resistant to bending - the stress in uprights - diagonal tension fields
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