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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Main Authors: | , , , , |
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Format: | Article |
Published: |
Penerbit Akademia Baru
2017
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Subjects: | |
Online Access: | http://eprints.utm.my/id/eprint/76384/ https://www.scop-us.com/inward/record.uri?eid=2-s2.0-85042793816&partnerID=40&md5=12b43b5cdf155aabe382e681d4d62778 |
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Institution: | Universiti Teknologi Malaysia |