The design and analyses of a subsonic rocket was carried out with the utilization of CFD. The effects of several critical parameters on the rocket performance were investigated. An increment in Mach number at approximately 30% results in an increment of drag coefficient nearly 68%. Changing the turbulence intensity does not make any significant difference on drag coefficient. The drag coefficient obtained from k-ω is higher than that of obtained from k-ω SST.
Bu makaleye şu şekilde atıfta bulunabilirsiniz(To cite to this article): Aytaç F. Z. and Yücel N., "Development of a design methodology for a centrifugal compressor with the utilization of CFD",
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