Study of potential aerodynamic benefits from spanwise blowing at wingtip [microform] / Raymond E. Mineck.

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Bibliographic Details
Online Access: Click here to view online
Main Author: Mineck, Raymond E.
Corporate Author: Langley Research Center
Format: Government Document Microfilm Book
Language:English
Published: Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], [1995]
Series:NASA technical paper ; 3515.
Subjects:

MARC

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245 1 0 |a Study of potential aerodynamic benefits from spanwise blowing at wingtip  |h [microform] /  |c Raymond E. Mineck. 
260 |a Hampton, Va. :  |b National Aeronautics and Space Administration, Langley Research Center ;  |a [Springfield, Va.] :  |b [National Technical Information Service, distributor],  |c [1995] 
300 |a 1 volume. 
336 |a text  |b txt  |2 rdacontent. 
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490 1 |a NASA technical paper ;  |v 3515. 
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500 |a Shipping list number: 95-0744-M. 
533 |a Microfiche.  |b [Washington, D.C. :  |c National Aeronautics and Space Administration,  |c 1995]  |e 2 microfiches. 
650 7 |a Aerodynamic drag.  |2 nasat. 
650 7 |a Aerodynamics.  |2 nasat. 
650 7 |a Commercial aircraft.  |2 nasat. 
650 7 |a Lift.  |2 nasat. 
650 7 |a Navier-Stokes equation.  |2 nasat. 
650 7 |a Spanwise blowing.  |2 nasat. 
650 7 |a Subsonic speed.  |2 nasat. 
650 7 |a Swept wings.  |2 nasat. 
650 7 |a Wind tunnel tests.  |2 nasat. 
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830 0 |a NASA technical paper ;  |v 3515.  |0 http://id.loc.gov/authorities/names/n42017381. 
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