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Analysis of Flow around Conical, Ogive Nose Cones in Hypersonic Space ShuttleBy Murali K., Sabik Nainar A, Maheshwaran .
Abstract: Hypersonic flow is a high Mach number regime used to distinguish flow fields, phenomena and problems appearing at flight speed far greater than the speed of sound. In high speed flows shock waves are formed during the flow. High speed flow have high energy level, thus dissipate large amount of heat, resulting in high temperatures, which may even burn the surface. The nose cone should be built with an outer …
Published in Research & Reviews : Journal of Space Science & Technology · Vol. 4, Issue 1, 2015 · pp. 1–7 Read article →