Numerical computation of 3-dimensional supersonic flow field over seamless missiles
Investigation of the flow field surrounding supersonic non uniform flying body is a challenge to the aerodynamics researchers. Such investigation by the traditional experimental technique in the wind tunnel is a time consuming and costly. The alternative option is the CFD simulation. This work deals...
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| Main Authors: | , , , |
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| Format: | Article |
| Published: |
Indian Society for Education and Environment
2014
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| Online Access: | https://www.scopus.com/inward/record.uri?eid=2-s2.0-84908885167&partnerID=40&md5=4edd27c3fbc791057d0b7258a41c7884 http://eprints.utp.edu.my/32021/ |
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| Institution: | Universiti Teknologi Petronas |