Flight determination of the aerodynamic stability and control characteristics of the NASA SGS 1-36 sailplane in the conventional and deep stall angles-of-attack of between -5 and 75 degrees [microform] / by Faramarz A. Mahdavi, Dral R. Sandlin.

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Bibliographic Details
Main Author:	Mahdavi, Faramarz A.
Corporate Author:	United States. National Aeronautics and Space Administration
Other Authors:	Sandlin, Dral R.
Format:	Government Document Microfilm Book
Language:	English
Published:	San Luis Obispo, Calif. : [Washington, DC] : [Springfield, Va.] : California Polytechnic State University, Aeronautical Engineering Dept. ; [National Aeronautics and Space Administration] ; [National Technical Information Service, distributor], [1984]
Series:	NASA contractor report ; NASA CR-176962.
Subjects:	Aerodynamic stability. Aerodynamic stalling. Aircraft performance. Angle of attack. Flight tests. Gliders. Wind tunnel tests. Angle of attack (Aerodynamics)

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.26:176962
NAS 1.26:176962	Restricted Place a Hold