A Non-Axisymmetric Linearized Supersonic Wave Drag Analysis: Mathematical Theory
Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
ISBN:  

9781725006577


Pages:   38
Publication Date:   09 August 2018
Format:   Paperback
Availability:   Available To Order   Availability explained
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A Non-Axisymmetric Linearized Supersonic Wave Drag Analysis: Mathematical Theory


Overview

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...

Full Product Details

Author:   National Aeronaut Administration (Nasa)
Publisher:   Createspace Independent Publishing Platform
Imprint:   Createspace Independent Publishing Platform
Dimensions:   Width: 21.60cm , Height: 0.20cm , Length: 28.00cm
Weight:   0.115kg
ISBN:  

9781725006577


ISBN 10:   172500657
Pages:   38
Publication Date:   09 August 2018
Audience:   General/trade ,  General
Format:   Paperback
Publisher's Status:   Active
Availability:   Available To Order   Availability explained
We have confirmation that this item is in stock with the supplier. It will be ordered in for you and dispatched immediately.

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