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...
Main Authors: | , |
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Format: | Research Report |
Published: |
2008
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Online Access: | http://hdl.handle.net/10356/6836 |
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author | Atta, E. H. Yeung, Wai Hung. |
author2 | School of Mechanical and Production Engineering |
author_facet | School of Mechanical and Production Engineering Atta, E. H. Yeung, Wai Hung. |
author_sort | Atta, E. H. |
collection | NTU |
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. |
first_indexed | 2024-10-01T03:38:07Z |
format | Research Report |
id | ntu-10356/6836 |
institution | Nanyang Technological University |
last_indexed | 2024-10-01T03:38:07Z |
publishDate | 2008 |
record_format | dspace |
spelling | ntu-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 |
spellingShingle | DRNTU::Engineering::Aeronautical engineering::Aerodynamics Atta, E. H. Yeung, Wai Hung. Computational methods of missile aerodynamics |
title | 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_short | Computational methods of missile aerodynamics |
title_sort | computational methods of missile aerodynamics |
topic | DRNTU::Engineering::Aeronautical engineering::Aerodynamics |
url | http://hdl.handle.net/10356/6836 |
work_keys_str_mv | AT attaeh computationalmethodsofmissileaerodynamics AT yeungwaihung computationalmethodsofmissileaerodynamics |