Mach 6 Wind Tunnel Tests Reveal Asymmetric Fin-Cone Boundary Layer Transition Dynamics
Experiments in a Mach 6 Ludwieg tube reveal how expansion waves and vortex interactions govern boundary layer transition on an ...
Tag: hypersonic aerodynamics
Hypersonic Heat Flux Model Resolves Vibrational and Catalytic Surface Effects
Computational simulations reveal that incomplete vibrational accommodation and finite-rate wall catalysis significantly shift peak aerothermal heating on hypersonic compression corners ...
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