Pages that link to "Item:Q605131"
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The following pages link to Effect of disturbances at inlet on hypersonic boundary layer transition on a blunt cone at small angle of attack (Q605131):
Displaying 4 items.
- Effect of the cone nose bluntness and the ultrasonically absorptive coating on transition in a hypersonic boundary layer (Q665591) (← links)
- Stability analysis and transition prediction of hypersonic boundary layer over a blunt cone with small nose bluntness at zero angle of attack (Q940281) (← links)
- Mechanism of transition in a hypersonic sharp cone boundary layer with zero angle of attack (Q940372) (← links)
- Applications of EPSE method for predicting crossflow instability in swept-wing boundary layers (Q2011560) (← links)