Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
By: Scott P. Fears, Holly M. Ross, and Thomas M. Moul.
Contributors: Moul, Thomas M.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 4640.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Aerodynamic stability.; Angle of attack.; Aspect ratio.; Flight control.; Flight stability tests.; Leading edge flaps.; Low speed.; Planforms.; Stabilizers (Fluid dynamics); Tail assemblies.; Trailing edge flaps.; Wind tunnel tests.; Wing profiles.
Other titles: Low speed wind tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0058-M.

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