Investigation Of The Downwash And Wake Behind A Triangular Wing Of Aspect Ratio 4 At Subsonic And Supersonic Mach Numbers PDF Download

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Investigation of the Downwash and Wake Behind a Triangular Wing of Aspect Ratio 4 at Subsonic and Supersonic Mach Numbers

Investigation of the Downwash and Wake Behind a Triangular Wing of Aspect Ratio 4 at Subsonic and Supersonic Mach Numbers
Author: Harold J. Walker
Publisher:
Total Pages: 32
Release: 1950
Genre: Airplanes
ISBN:

Download Investigation of the Downwash and Wake Behind a Triangular Wing of Aspect Ratio 4 at Subsonic and Supersonic Mach Numbers Book in PDF, ePub and Kindle

The effects of Mach number in the ranges between 0.50 and 0.95 and between 1.09 and 1.29 on the characteristics of the downwash and on the location of the wake behind a triangular wing of aspect ratio 4 have been determined from semispan model tests.


Index of NACA Technical Publications

Index of NACA Technical Publications
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 388
Release: 1959
Genre: Aeronautics
ISBN:

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Report

Report
Author:
Publisher:
Total Pages: 1138
Release: 1958
Genre: Aeronautics
ISBN:

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Report

Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Total Pages: 70
Release: 1958
Genre: Aeronautics
ISBN:

Download Report Book in PDF, ePub and Kindle