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Leading-edge deflection optimization for a highly swept arrow-wing configuration / Paul L. Coe, Jr., Jarrett K. Huffman, and James W. Fenbert.
- Format:
- Book
- Government document
- Author/Creator:
- Coe, Paul L., author.
- Huffman, Jarrett K., author.
- Fenbert, James W., author.
- Series:
- NASA technical paper ; 1777.
- NASA technical paper ; 1777
- Language:
- English
- Subjects (All):
- Aerodynamics.
- Airplanes--Wings, Swept-back.
- Airplanes.
- Leading edges (Aerodynamics).
- aerodynamics.
- Genre:
- Online resources.
- Physical Description:
- 1 online resource (56 pages) : illustrations
- Place of Publication:
- [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
- Notes:
- Title from title screen (viewed on August 25, 2016).
- "December 1980."
- "Performing Organization: NASA Langley Research Center"--Report documentation page
- Includes bibliographical references (pages 55-56).
- Other Format:
- Print version: Coe, Paul L. Leading-edge deflection optimization for a highly swept arrow-wing configuration
- Microfiche version: Coe, Paul L. Leading-edge deflection optimization for a highly swept arrow-wing configuration
- OCLC:
- 760918532
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