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A Wind-tunnel Test Technique for Measuring the Dynamic Rotary Stability Derivatives Including the Cross Derivatives at High Mach Numbers

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Release : 1955
Genre : Aerodynamics, Supersonic
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Book Synopsis A Wind-tunnel Test Technique for Measuring the Dynamic Rotary Stability Derivatives Including the Cross Derivatives at High Mach Numbers by : Benjamin H. Beam

Download or read book A Wind-tunnel Test Technique for Measuring the Dynamic Rotary Stability Derivatives Including the Cross Derivatives at High Mach Numbers written by Benjamin H. Beam. This book was released on 1955. Available in PDF, EPUB and Kindle. Book excerpt: A method is described for measuring the dynamic stability derivatives of a model airplane in a wind tunnel. The characteristics features of this system are that single-degree-of-freedom oscillations were used to obtain combinations of rolling, yawing, and pitching motions; that the oscillations were excited and controlled by velocity feedback which permitted operation under conditions unfavorable for more conventional types of oscillatory testing; and that data processing was greatly simplified by using analog computer elements in the strain-gage circuitry.

NASA Technical Note

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Author :
Release : 1972
Genre :
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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by . This book was released on 1972. Available in PDF, EPUB and Kindle. Book excerpt:

Prediction of Downwash Behind Swept-wing Airplanes at Subsonic Speed

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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.

Technical Note - National Advisory Committee for Aeronautics

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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:

U.S. Government Research Reports

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Author :
Release : 1955
Genre : Science
Kind : eBook
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Book Synopsis U.S. Government Research Reports by :

Download or read book U.S. Government Research Reports written by . This book was released on 1955. Available in PDF, EPUB and Kindle. Book excerpt:

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