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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Bibliographic Details
Main Authors: Al-Kayiem, H.H., Hussein, A.K., Jaleel, J.M., Hussain, S.H.
Format: Article
Published: Indian Society for Education and Environment 2014
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
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