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- W4362727736 abstract "A blunt body re-entry capsule requires favourable aerodynamic and aero thermodynamic characteristics throughout its atmospheric re-entry period. Incorporation of undulations on a re-entry vehicle is one of the plausible methods that is expected to improve the Aero-thermodynamic features of the re-entry vehicle. The present study deals with the steady-state computational analysis for a two dimensional (2D) undulated Crew Exploration Vehicle (CEV), to understand the effect of undulations on the aerodynamic and aero thermodynamic characteristics of the re-entry capsule. In this work, computational investigations were carried out for two different Mach regimes, supersonic of M3 and hypersonic of M7, and the angle of attack (AOA) was varied between 0° and 15°. Analysis were mainly focused on the parameters like, shock stand-off distance, nature of shock wave formation and recirculation region of the flow. The result shows that a average reduction of 14.9% heat flux inM3 and 26.6% heat flux reduction in M7 regime at 15° AOA for an undulated re-entry capsule." @default.
- W4362727736 created "2023-04-10" @default.
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- W4362727736 date "2023-01-01" @default.
- W4362727736 modified "2023-09-27" @default.
- W4362727736 title "Computational Aero thermodynamic Study on Orion and Undulated Reentry Capsules" @default.
- W4362727736 doi "https://doi.org/10.1007/978-981-19-6970-6_23" @default.
- W4362727736 hasPublicationYear "2023" @default.
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