Application of a numerical procedure to stress analysis of stringer-reinforced panels Metadata
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Title
- Main Title Application of a numerical procedure to stress analysis of stringer-reinforced panels
- Series Title NACA Wartime Reports
- Series Title NACA Advanced Restricted Reports
Creator
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Author: Kempner, JosephCreator Type: Personal
Contributor
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Originator: Langley Aeronautical LaboratoryContributor Type: OrganizationContributor Info: National Advisory Committee for Aeronautics. Langley Aeronautical Lab
Date
- Creation: 1945-03
Language
- English
Description
- Content Description: From Introduction: "In the present paper a numerical procedure for the stress analysis of flat-sheet and stringer combinations of arbitrary construction and loading is presented and applied to axially loaded panels and to the reinforced covers of box beams."
- Physical Description: 23 p. : ill.
Subject
- Keyword: panels
- Keyword: stress analyses
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
- Accession or Local Control No: 93R21828
- URL: http://hdl.handle.net/2060/19930092538
- Report No.: NACA-WR-L-11
- Report No.: NACA-ARR-L5C09a
- Center for AeroSpace Information Number: 19930092538
- Archival Resource Key: ark:/67531/metadc60971