Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
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Author
Contributions
- Moul, Thomas M. - Contributor
- United States. National Aeronautics and Space Administration. - Contributor
Publication
1995 - National Aeronautics and Space Administration, [Washington, DC, District of Columbia
Language
English
Word Count
36,250 words, Guess
Page Count
145 pages
Physical Format
Microform
Identifiers
- OCLC Control Number34127880
- Open LibraryOL17032232M
Alternate Titles
- Low speed wind tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50.̊
Subjects
Topics
StabilityPlanformsLow speedArrow wingsAspect ratioWing profilesFlight controlAngle of attackTail assembliesWind tunnel testsLeading edge flapsTrailing edge flapsAerodynamic stabilityFlight stability testsStabilizers (Fluid dynamics)
Series Statement
- NASA technical memorandum -- 4640.
Other Editions
- Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
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