Leading-edge deflection optimization for a highly swept arrow-wing configuration /
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Author / Creator: | Coe, Paul L., author. |
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Imprint: | [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980. |
Description: | 1 online resource (56 pages) : illustrations. |
Language: | English |
Series: | NASA technical paper ; 1777 NASA technical paper ; 1777. |
Subject: | |
Format: | E-Resource U.S. Federal Government Document Book |
URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/10914234 |
Other authors / contributors: | 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. |
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Notes: | Title from title screen (viewed on Aug. 25, 2016). "December 1980." "Performing Organization: NASA Langley Research Center"--Report documentation page. Includes bibliographical references (pages 55-56). Technical paper. National Aeronautics and Space Administration 533-01-43-02 L-13820 |
Other form: | 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 |
GPO item no.: | 0830-H-15 (online) |
Govt.docs classification: | NAS 1.60:1777 |
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