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Experimental Investigation of Flutter of a Propeller with Clark Y Section Operating at Zero Forward Velocity at Positive and Negative Blade-angle Settings

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Release : 1949
Genre : Aerofoils
Kind : eBook
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Book Synopsis Experimental Investigation of Flutter of a Propeller with Clark Y Section Operating at Zero Forward Velocity at Positive and Negative Blade-angle Settings by : John E. Baker

Download or read book Experimental Investigation of Flutter of a Propeller with Clark Y Section Operating at Zero Forward Velocity at Positive and Negative Blade-angle Settings written by John E. Baker. This book was released on 1949. Available in PDF, EPUB and Kindle. Book excerpt: The highest flutter speeds were found in the vicinity of the angle of zero aerodynamic moment and the flutter speed increased considerably in this region with decreasing pressure. Over the rest of the pitch range, the flutter speeds were much lower and varied little with pressure.

Technical Note - National Advisory Committee for Aeronautics

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Author :
Release : 1955
Genre : Aeronautics
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Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics. This book was released on 1955. Available in PDF, EPUB and Kindle. Book excerpt:

Bibliography of Technical Reports

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Author :
Release : 1950
Genre : Science
Kind : eBook
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Book Synopsis Bibliography of Technical Reports by :

Download or read book Bibliography of Technical Reports written by . This book was released on 1950. Available in PDF, EPUB and Kindle. Book excerpt:

Prediction of Downwash Behind Swept-wing Airplanes at Subsonic Speed

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Author :
Release : 1955
Genre : Airplanes
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Book Synopsis Prediction of Downwash Behind Swept-wing Airplanes at Subsonic Speed by : John DeYoung

Download or read book Prediction of Downwash Behind Swept-wing Airplanes at Subsonic Speed written by John DeYoung. This book was released on 1955. Available in PDF, EPUB and Kindle. Book excerpt: A rapid method for estimating the downwash behind swept-wing airplanes is presented. The basic assumption is that of a flat horizontal sheet of vortices trailing behind the wing. The integrations for the downwash are handled in a manner similar to both Multhopp's and Weissinger's approximate integrations in their span-loading calculations. The principal effects of rolling-up of the wake are treated as corrections to the flat-sheet wake. A simple approximate correction for the effect of the fuselage is applied. The agreement with available experimental data taken behind airplane models is good. Computing forms are included together with charts of pertinent functions, so as to enable simple direct application.

A Selected Listing of NASA Scientific and Technical Reports for ...

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Author :
Release : 1949
Genre : Aeronautics
Kind : eBook
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Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :

Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by . This book was released on 1949. Available in PDF, EPUB and Kindle. Book excerpt:

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