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- W3008924963 abstract "Highly blunt configurations are generally used to decelerate spacecraft during reentry, but these configurations exhibit very poor aerodynamics characteristics, i.e., low lift-to-drag ratio. Attachment of flap may improve the aerodynamic characteristics of the blunt cone. Detailed analysis of the effect of ramp and flap over the blunt cone at supersonic speed has been done adopting numerical studies. Three-dimensional, steady, viscous flow through reentry capsule has been simulated using commercial CFD package FLUENTv15 and adopting k-ω (SST) turbulence model. Effect of flap angle on the base flow and the stability of the capsule have been studied at different altitudes using computational studies." @default.
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- W3008924963 date "2020-01-01" @default.
- W3008924963 modified "2023-09-26" @default.
- W3008924963 title "Effects of Flap on the Reentry Aerodynamics of a Blunt Cone" @default.
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- W3008924963 doi "https://doi.org/10.1007/978-981-15-1892-8_22" @default.
- W3008924963 hasPublicationYear "2020" @default.
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