Effect of leading-edge load constraints on the design and performance of supersonic wings
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- Created Date
- 1985
- Description
Prepared at Langley Research Center.
"July 1985"--Cover.
Includes bibliographical references (p. 7).
- Creator
Darden, Christine M
- Partner
- HathiTrust
- Contributing Institution
- University of Illinois
- Publisher
- Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service
- Subjects
- Airplanes--Wings--Design and construction
Aerodynamics, Supersonic
Aerodynamic load
Leading edges (Aerodynamics)
Airplanes--Wings--Testing--Statistics - Type
- text
- Format
- Language materialElectronic resourceStatistics.
- Language
- English
- Rights
- Public domain. Learn more at http://www.hathitrust.org/access_use
- Chicago citation style
- Darden, Christine M. Effect of leading-edge load constraints on the design and performance of supersonic wings. 1985. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011425581. (Accessed March 28, 2024.)
- APA citation style
- Darden, Christine M, (1985) Effect of leading-edge load constraints on the design and performance of supersonic wings. Retrieved from the Digital Public Library of America, http://catalog.hathitrust.org/Record/011425581
- MLA citation style
- Darden, Christine M. Retrieved from the Digital Public Library of America <http://catalog.hathitrust.org/Record/011425581>.