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Aerodynamic Characteristics of Unguided Artillery Projectile
Abstract:
The paper presents results of investigation of a flow over unguided artillery projectile in order to understand variation of flow parameters past a 155 mm artillery projectile M107 and the performance of the computational code. Furthermore; static aerodynamic coefficients were calculated. The flow around projectile was solved as 3-D unsteady compressible flow.
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165-168
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Online since:
July 2014
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© 2014 Trans Tech Publications Ltd. All Rights Reserved
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