Computational methods of missile aerodynamics

A computational method has been developed for the prediction of missile flow fields with emphasis on subsonic and transonic flight-conditions. The computational method is based on the thin shear layer formulation of the Navier-Stokes equations and a finite volume Runge-Kutta time marching algorithm...

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Bibliographic Details
Main Authors:	Atta, E. H., Yeung, Wai Hung.
Other Authors:	School of Mechanical and Production Engineering
Format:	Research Report
Published:	2008
Subjects:	DRNTU::Engineering::Aeronautical engineering::Aerodynamics
Online Access:	http://hdl.handle.net/10356/6836
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Institution:	Nanyang Technological University

id	sg-ntu-dr.10356-6836
record_format	dspace
spelling	sg-ntu-dr.10356-68362020-06-01T10:44:38Z Computational methods of missile aerodynamics Atta, E. H. Yeung, Wai Hung. School of Mechanical and Production Engineering DRNTU::Engineering::Aeronautical engineering::Aerodynamics A computational method has been developed for the prediction of missile flow fields with emphasis on subsonic and transonic flight-conditions. The computational method is based on the thin shear layer formulation of the Navier-Stokes equations and a finite volume Runge-Kutta time marching algorithm. ARP-61-91 2008-09-17T14:35:30Z 2008-09-17T14:35:30Z 1993 1993 Research Report http://hdl.handle.net/10356/6836 Nanyang Technological University application/pdf
institution	Nanyang Technological University
building	NTU Library
country	Singapore
collection	DR-NTU
topic	DRNTU::Engineering::Aeronautical engineering::Aerodynamics
spellingShingle	DRNTU::Engineering::Aeronautical engineering::Aerodynamics Atta, E. H. Yeung, Wai Hung. Computational methods of missile aerodynamics
description	A computational method has been developed for the prediction of missile flow fields with emphasis on subsonic and transonic flight-conditions. The computational method is based on the thin shear layer formulation of the Navier-Stokes equations and a finite volume Runge-Kutta time marching algorithm.
author2	School of Mechanical and Production Engineering
author_facet	School of Mechanical and Production Engineering Atta, E. H. Yeung, Wai Hung.
format	Research Report
author	Atta, E. H. Yeung, Wai Hung.
author_sort	Atta, E. H.
title	Computational methods of missile aerodynamics
title_short	Computational methods of missile aerodynamics
title_full	Computational methods of missile aerodynamics
title_fullStr	Computational methods of missile aerodynamics
title_full_unstemmed	Computational methods of missile aerodynamics
title_sort	computational methods of missile aerodynamics
publishDate	2008
url	http://hdl.handle.net/10356/6836
_version_	1681056810304274432

Computational methods of missile aerodynamics

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