Minimum-mass design of filamentary composite panels under combined loads : design procedure based on a rigorous buckling analysis
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- Created Date
- 1977
- Description
Issued July 1977.
Includes bibliographical references.
- Creator
Stroud, W. Jefferson
- Partner
- HathiTrust
- Contributing Institution
- University of Illinois
- Publisher
- Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service
- Subjects
- Elastic plates and shells
Plates (Engineering)--Design and construction
Buckling (Mechanics)--Computer simulation
Fibrous composites--Computer simulation - Type
- text
- Format
- Language materialElectronic resource
- Language
- English
- Rights
- Public domain. Learn more at http://www.hathitrust.org/access_use
- Chicago citation style
- Stroud, W. Jefferson. Minimum-mass design of filamentary composite panels under combined loads : design procedure based on a rigorous buckling analysis. 1977. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444096. (Accessed April 19, 2024.)
- APA citation style
- Stroud, W. Jefferson, (1977) Minimum-mass design of filamentary composite panels under combined loads : design procedure based on a rigorous buckling analysis. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011444096
- MLA citation style
- Stroud, W. Jefferson. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011444096>.