Investigation of Heat and Drag Reduction Induced by Forward-Facing Cavity in Hypersonic Flow

The design of heat and drag reduction systems for hypersonic vehicles has garnered widespread global attention. In this study, the Navier–Stokes equations and the SST k-ω turbulence model are employed to establish a simulation model for heat and drag reduction induced by a forward-facing cavity. The...

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Bibliographic Details
Main Authors: Ning Ding, Jianlong Chang, Junhui Liu
Format: Article
Language:English
Published: MDPI AG 2025-04-01
Series:Aerospace
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Online Access:https://www.mdpi.com/2226-4310/12/5/394
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