Numerical Simulations on Aerodynamic Characteristics of a Guided Rocket Projectile

DOI

10.2991/icmemtc-16.2016.199How to use a DOI?

Keywords

Aerodynamics characteristics; guided rocket projectile; CFD.

Abstract

Aerodynamic characteristics of a guided rocket projectile are numerically simulated. Simulations are performed in a range of flight conditions using a commercial CFD software FLUENT, and variations of lift coefficients and drag coefficients with Mach numbers and angles of attack were demonstrated. The numerical results also indicate that the angle of canard deflection has significant influence on the flow field near tailfins.

Copyright

© 2016, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Jiazhong Peng
AU  - Liangyu Zhao
AU  - Longyin Jiao
PY  - 2016/04
DA  - 2016/04
TI  - Numerical Simulations on Aerodynamic Characteristics of a Guided Rocket Projectile
BT  - Proceedings of the 2016 3rd International Conference on Materials Engineering, Manufacturing Technology and Control
PB  - Atlantis Press
SP  - 1004
EP  - 1007
SN  - 2352-5401
UR  - https://doi.org/10.2991/icmemtc-16.2016.199
DO  - 10.2991/icmemtc-16.2016.199
ID  - Peng2016/04
ER  -