Pages that link to "Item:Q5149503"
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The following pages link to Dilatational-wave-induced aerodynamic cooling in transitional hypersonic boundary layers (Q5149503):
Displaying 7 items.
- Effect of the cone nose bluntness and the ultrasonically absorptive coating on transition in a hypersonic boundary layer (Q665591) (← links)
- Mechanism of unsteady aerodynamic heating with sudden change in surface temperature (Q1016180) (← links)
- Influence of intense surface cooling on hypersonic viscous flow past a delta wing (Q1304554) (← links)
- Numerical Investigations of Effusion Cooling in Hypersonic Boundary-Layer Flow (Q3122274) (← links)
- Newly identified principle for aerodynamic heating in hypersonic flows (Q4685472) (← links)
- Instabilities and transition in cooled wall hypersonic boundary layers (Q5857817) (← links)
- Second-order analysis of hypersonic boundary-layer stability (Q6644875) (← links)