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:

MARC

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245 1 0 |a 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  |h [microform] /  |c by Faramarz A. Mahdavi, Dral R. Sandlin. 
260 |a San Luis Obispo, Calif. :  |b California Polytechnic State University, Aeronautical Engineering Dept. ;  |a [Washington, DC] :  |b [National Aeronautics and Space Administration] ;  |a [Springfield, Va.] :  |b [National Technical Information Service, distributor],  |c [1984] 
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533 |a Microfiche.  |b [Washington, D.C. :  |c National Aeronautics and Space Administration,  |d 1986]  |e 2 microfiches. 
650 7 |a Aerodynamic stability.  |2 nasat. 
650 7 |a Aerodynamic stalling.  |2 nasat. 
650 7 |a Aircraft performance.  |2 nasat. 
650 7 |a Angle of attack.  |2 nasat. 
650 7 |a Flight tests.  |2 nasat. 
650 7 |a Gliders.  |2 nasat. 
650 7 |a Wind tunnel tests.  |2 nasat. 
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