Slender Body Theory Based On Approximate Solution Of The Transonic Flow Equation

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Slender-body Theory Based on Approximate Solution of the Transonic Flow Equation

Slender-body Theory Based on Approximate Solution of the Transonic Flow Equation
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Total Pages : 252
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ISBN-10 : NASA:31769000420011
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Book Synopsis Slender-body Theory Based on Approximate Solution of the Transonic Flow Equation by : John R. Spreiter

Download or read book Slender-body Theory Based on Approximate Solution of the Transonic Flow Equation written by John R. Spreiter and published by . This book was released on 1959 with total page 252 pages. Available in PDF, EPUB and Kindle. Book excerpt: Approximate solutions of the nonlinear equations of the small disturbance theory of transonic flow are found for the pressure distribution on pointed slender bodies of revolution for flows with free-stream Mach number 1, and for flows that are either purely subsonic or purely supersonic. These results are obtained by application of a method based on local linearization that was introduced recently in the analysis of similar problems in low-dimensional flows. The theory is developed for bodies of arbitrary shapes, and specific results are given for cone-cylinders and for parabolic-arc bodies at zero angle of attack. All results are compared either with existing theoretical results or with experimental data.


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Slender-body Theory Based on Approximate Solution of the Transonic Flow Equation
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