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Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50̊ [microform] / Scott P. Fears, Holly M. Ross, and Thomas M. Moul.

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Bibliographic Details
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Main Author:	Fears, Scott P.
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Moul, Thomas M.
Other title:	Low speed wind tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50̊
Format:	Government Document Book
Language:	English
Published:	[Washington, DC] : [Springfield, Va.] : [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], [1995]
Series:	NASA technical memorandum ; 4640.
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.

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Call Number:	NAS 1.15:4640
NAS 1.15:4640	Available

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:4640
NAS 1.15:4640	Restricted Place a Hold