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Computations of projectile Magnus effect at transonic velocities

โœ Scribed by NIETUBICZ, C. J.; STUREK, W. B.; HEAVEY, K. R.


Book ID
126674667
Publisher
American Institute of Aeronautics and Astronautics
Year
1985
Tongue
English
Weight
861 KB
Volume
23
Category
Article
ISSN
0001-1452

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The aerodynamic performance of a spinning secant-ogive-cylinder-boattail (SOCBT) projectile in the transonic regime is numerically investigated. In the present study, a porous surface is applied to improve the projectile performance. The computed results show that the porous surface on the boattail