Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊
By: Holly M. Ross, Scott P. Fears, and Thomas M. Moul.
Contributors: Fears, Scott P.; Moul, Thomas M.; Langley Research Center.
Series: NASA technical memorandum -- 4671.
Publisher: National Aeronautics and Space Administration, Langley Research Center; Available from the National Technical Information Service
Published: 1995
Place of publication: Hampton, Va; [Springfield, VA
Language: eng
Subjects: Angle of attack.; Arrow wings.; Dynamic characteristics.; Low aspect ratio wings.; Low speed.; Radar cross sections.; Sideslip.; Tailless aircraft.; Wind tunnel tests.
Other titles: Low speed wind tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 ̊
Notes: Shipping List #: 96-0637-M.

Also available via Internet from the NASA Technical Report Server web site. Address as of 6/21/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19960003028%5F1996103028.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995]. 2 microfiches.