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CFD Analysis of Rocket Nose Cone Drag by amoaghashesha1406 is a document available to read on EtoBox.
This conference paper presents a computational fluid dynamics (CFD) analysis of the drag force for different rocket nose cone designs, focusing on subsonic speeds from Mach 0.05 to 0.62. The study evaluates four nose cone shapes: tangent, parabolic, ellipsoidal, and conic, with results indicating that the elliptical shape offers the best aerodynamic performance, followed by tangent and parabolic shapes, while the conic design shows the worst performance. The authors suggest future work to validate the simul
- Author
- amoaghashesha1406
- Language
- EN