Flow Field Investigations and Aerodynamic Characteristics of Artillery Projectile

DOI

10.2991/eame-15.2015.73How to use a DOI?

Keywords

artillery projectile; aerodynamic coefficients; CFD;ANSYS FLUENT

Abstract

This paper describes a computational study to determine the aerodynamic coefficients at subsonic and supersonic speeds using an unstructured flow solver. The paper presents results of investigation of a flow over 155 mm artillery projectile M107 and the performance of the ANSYS FLUENT computational code. The flow around projectile was solved as 3-D unsteady compressible flow.

Copyright

© 2015, 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  - M.E. Wessam
AU  - Z.H. Chen
PY  - 2015/07
DA  - 2015/07
TI  - Flow Field Investigations and Aerodynamic Characteristics of Artillery Projectile
BT  - Proceedings of the 2015 International Conference on Electrical, Automation and Mechanical Engineering
PB  - Atlantis Press
SP  - 267
EP  - 270
SN  - 2352-5401
UR  - https://doi.org/10.2991/eame-15.2015.73
DO  - 10.2991/eame-15.2015.73
ID  - Wessam2015/07
ER  -