- Additional Authors
- Description
- 1 online resource (56 pages) : illustrations.
- Series Statement
- NASA technical paper ; 1777
- Uniform Title
- NASA technical paper ; 1777.
- Subject
- Note
- Title from title screen (viewed on Aug. 25, 2016).
- "December 1980."
- "Performing Organization: NASA Langley Research Center"--Report documentation page.
- Bibliography (note)
- Includes bibliographical references (pages 55-56).
- Type of Report (note)
- Funding (note)
- National Aeronautics and Space Administration
- Call Number
- GPO Internet NAS 1.60:1777
- OCLC
- marcive760918532
- Author
Coe, Paul L., author.
- Title
Leading-edge deflection optimization for a highly swept arrow-wing configuration / Paul L. Coe, Jr., Jarrett K. Huffman, and James W. Fenbert.
- Publisher
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
- Type of Content
text
- Type of Medium
computer
- Type of Carrier
online resource
- Series
NASA technical paper ; 1777
NASA technical paper ; 1777.
- Bibliography
Includes bibliographical references (pages 55-56).
- Type Of Report
Technical paper.
- Funding
National Aeronautics and Space Administration 533-01-43-02 L-13820
- Connect to:
- Added Author
Huffman, Jarrett K., author.
Fenbert, James W., author.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
- Other Form:
Print version: Coe, Paul L. Leading-edge deflection optimization for a highly swept arrow-wing configuration (OCoLC)7503108
Microfiche version: Coe, Paul L. Leading-edge deflection optimization for a highly swept arrow-wing configuration (OCoLC)711544844
- Gpo Item No.
0830-H-15 (online)
- Sudoc No.
NAS 1.60:1777