A Non-Axisymmetric Linearized Supersonic Wave Drag Analysis PDF Download
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Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725006577
Category :
Languages : en
Pages : 38
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Book Description
A Mathematical theory is developed to perform the calculations necessary to determine the wave drag for slender bodies of non-circular cross section. The derivations presented in this report are based on extensions to supersonic linearized small perturbation theory. A numerical scheme is presented utilizing Fourier decomposition to compute the pressure coefficient on and about a slender body of arbitrary cross section. Barnhart, Paul J. Glenn Research Center NASA-CR-198430, NAS 1.26:198430, E-10030 NAS3-27186; RTOP 505-60-00...
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781725006577
Category :
Languages : en
Pages : 38
Get Book Here
Book Description
A Mathematical theory is developed to perform the calculations necessary to determine the wave drag for slender bodies of non-circular cross section. The derivations presented in this report are based on extensions to supersonic linearized small perturbation theory. A numerical scheme is presented utilizing Fourier decomposition to compute the pressure coefficient on and about a slender body of arbitrary cross section. Barnhart, Paul J. Glenn Research Center NASA-CR-198430, NAS 1.26:198430, E-10030 NAS3-27186; RTOP 505-60-00...
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Category :
Languages : en
Pages : 22
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Author: Paul J. Barnhart
Publisher:
ISBN:
Category :
Languages : en
Pages : 172
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Author: C. H. Wilts
Publisher:
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Category : Aeronautics
Languages : en
Pages : 358
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Category : Government publications
Languages : en
Pages : 476
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Category : Aeronautics
Languages : en
Pages : 1278
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Category : Aeronautics
Languages : en
Pages : 1138
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Category : Aeronautics
Languages : en
Pages : 968
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Author: William Rees Sears
Publisher: Princeton University Press
ISBN: 1400877555
Category : Science
Languages : en
Pages : 778
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Book Description
Volume VI of the High Speed Aerodynamics and Jet Propulsion series. This volume includes: physical and mathematical aspects of high speed flows; small perturbation theory; supersonic and transonic small perturbation theory; higher order approximations; nonlinear subsonic and transonic flow theory; nonlinear supersonic steady-flow theory; characteristic methods; flows with shock waves. Originally published in 1954. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
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Category : Aeronautics
Languages : en
Pages :
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Book Description
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
