Abstract:A computational study has been carried out to investigate the air flow over a projectile provided with a triangular base at transonic and supersonic speeds. The study aims to discuss the effect of the triangular base on the air flow characteristics comparing with the flow over a typical projectile. One of the study main concerns is the drag since it is the key issue in the projectile range. Good agreement is noted when comparing the computational drag coefficients with the experimental work of Platou [11]. The… Show more
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