Numerical Computations of Transonic Critical AerodynamicBehavior of a Realistic Artillery Projectile
The determination of aerodynamic coefficients by shell designers is a critical step in the development of any projectile design. Of particular interest is the determination of the aerodynamic coefficients at transonic speeds. It is in this speed regime that the critical aerodynamic behavior occurs a...
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| Formato: | article |
| Lenguaje: | EN |
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Al-Khwarizmi College of Engineering – University of Baghdad
2009
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| Acceso en línea: | https://doaj.org/article/dbbf2ee1a6ed4006a3a4687959e7c768 |
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