Assessment of dual-point drag reduction for an executive-jet modified airfoil section
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Author
Contributions
- Mineck, Raymond E. - Contributor
- Langley Research Center. - Contributor
Publication
1996 - National Aeronautics and Space Administration, Langley Research Center, Hampton, Va, Virginia
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Physical Format
Microform
Identifiers
- OCLC Control Number40386607
- Open LibraryOL17581020M
Alternate Titles
- Assessment of dual point drag reduction for an executive-jet modified airfoil section.
Subjects
Series Statement
- NASA technical paper -- 3579.
Other Editions
- Assessment of dual-point drag reduction for an executive-jet modified airfoil section
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