Numerical Calculation of Transonic Flow about Slender Bodies of Revolution

Numerical Calculation of Transonic Flow about Slender Bodies of Revolution
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Total Pages : 44
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ISBN-10 : UIUC:30112106692665
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Book Synopsis Numerical Calculation of Transonic Flow about Slender Bodies of Revolution by : Frank R. Bailey

Download or read book Numerical Calculation of Transonic Flow about Slender Bodies of Revolution written by Frank R. Bailey and published by . This book was released on 1971 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: A relaxation method is described for the numerical solution of the transonic small disturbance equation for flow about a slender body of revolution. Results for parabolic arc bodies, both with and without an attached sting, are compared with wind-tunnel measurements for a free-stream Mach number range from 0.90 to 1.20. The method is also used to show the effects of wind-tunnel wall interference by including boundary conditions representing porous-wall and open-jet wind-tunnel test sections.

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Language: en
Pages: 44
Authors: Frank R. Bailey
Categories: Aerodynamics, Transonic
Type: BOOK - Published: 1971 - Publisher:

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A relaxation method is described for the numerical solution of the transonic small disturbance equation for flow about a slender body of revolution. Results for
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Summary: Approximate solutions of the nonlinear equations of the small disturbance theory of transonic flow are found for the pressure distribution on pointed s
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Pages: 82
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Categories: Aerodynamics, Transonic
Type: BOOK - Published: 1975 - Publisher:

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An analytical solution is obtained for the perturbation velocity potential for transonic flow about lifting wing-body configurations with order-one span-length
NASA Technical Note
Language: en
Pages: 418
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Calculative Techniques for Transonic Flows about Certain Classes of Wing-body Combinations, Phase 2
Language: en
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Type: BOOK - Published: 1972 - Publisher:

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Theoretical analysis and associated computer programs were developed for predicting properties of transonic flows about certain classes of wing-body combination