Wind-tunnel investigation of a full-scale canard-configured general aviation airplane /

Wind-tunnel investigation of a full-scale canard-configured general aviation airplane /

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Bibliographic Details
Main Authors: Yip, Long P, Yip, Long P. (Author)
Corporate Authors: United States National Aeronautics and Space Administration. Scientific and Technical Information Branch, Langley Research Center
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, March 1985
[Washington, D.C.] : 1985
Series:NASA technical paper ; 2382
NASA technical paper 2382
NASA technical paper 2382
Subjects:
Airplanes > Control surfaces
Airplanes > Wings, Canard > Testing
Flight control
Private flying
Rockets (Aeronautics) > Canard fins
Wind tunnels > Test gases
Aerodynamic balance
Aerodynamic characteristics
Canard configurations
Control stability
Control surfaces
General aviation aircraft
Wind tunnel tests
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Description
Item Description:Prepared at Langley Research Center
"March 1985."
"March 1985"--Cover
Physical Description:1 online resource (78 pages) : illustrations
1 volume
Also available via Internet from the NASA Technical Report Server web site. Address as of 10/20/04: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19850011615%5F1985011615.pdf; current access available via PURL
Format:Available via Internet from the NASA Technical Report Server web site. Address as of 10/20/04: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19850011615%5F1985011615.pdf; current access available via PURL
Bibliography:Includes bibliographical references (page 10)

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