Critical Compressive Stress for Outstanding Flanges Metadata
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Title
- Main Title Critical Compressive Stress for Outstanding Flanges
- Series Title NACA Special Reports
Creator
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Author: Lundquist, Eugene E.Creator Type: Personal
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Author: Stowell, Elbridge Z.Creator Type: Personal
Contributor
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Originator: Langley Aeronautical LaboratoryContributor Type: OrganizationContributor Info: NASA Langley Research Center
Date
- Creation: 1941-04
Language
- English
Description
- Content Description: "A chart is presented for the values of the coefficient in the formula for the critical compressive stress at which buckling may be expected to occur in outstanding flanges. These flanges are flat rectangular plates supported along the Loaded edges, supported and elastically restrained along one unloaded edge, and free along the other unloaded edge. The mathematical derivations of the formulas required for the construction of the chart are given" (p. 1).
- Physical Description: [27] p. : ill.
Subject
- Keyword: aircraft design
- Keyword: aircraft testing
- Keyword: aircraft performance
Collection
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Name: National Advisory Committee for Aeronautics CollectionCode: NACA
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Name: Technical Report Archive and Image LibraryCode: TRAIL
Institution
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Name: UNT Libraries Government Documents DepartmentCode: UNTGD
Rights
- Rights Access: public
- Rights License: pd
- Rights Statement: No Copyright, Unclassified, Unlimited, Publicly available
Resource Type
- Report
Format
- Text
Identifier
- URL: http://hdl.handle.net/2060/20090014138
- Report No.: NACA-SR-188
- Center for AeroSpace Information Number: 20090014138
- Report No.: NACA-TR-734
- Archival Resource Key: ark:/67531/metadc65027