Integration effects of D-shaped, underwing, aft-mounted, separate- flow, flow-through nacelles on a high-wing transport
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Author
Contributions
- Carlson, John R. - Contributor
- Pendergraft, Odis C. - Contributor
- United States. National Aeronautics and Space Administration. Scientific and Technical Information Division. - Contributor
Publication
1988 - National Aeronautics and Space Administration, Scientific and Technical Information Division, Washington, DC, District of Columbia
Language
English
Word Count
5,250 words, Guess
Page Count
21 pages
Physical Format
Microform
Identifiers
- OCLC Control Number22504872
- Open LibraryOL17096819M
Subjects
Topics
Series Statement
- NASA technical memorandum -- 4018
Other Editions
- Integration effects of D-shaped, underwing, aft-mounted, separate- flow, flow-through nacelles on a high-wing transport
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