Aerodynamic study of air flow over a curved fin rocket

This paper summarizes a study of the aerodynamic characteristics of a curved fin rocket. The study was conducted with the use of semi-empirical method and numerical simulation. The semi-empirical method was implemented with USAF DATCOM as a reference. The ANSYS Fluent was used for the numerical simu...

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Bibliographic Details
Main Authors: Dahalan, M. N., Suni, A. F., Ishak, I. S., Mohd., N. A. R. N., Mat, S.
Format: Article
Published: Penerbit Akademia Baru 2017
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Online Access:http://eprints.utm.my/id/eprint/76384/
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Institution: Universiti Teknologi Malaysia