Pages that link to "Item:Q940281"

The following pages link to Stability analysis and transition prediction of hypersonic boundary layer over a blunt cone with small nose bluntness at zero angle of attack (Q940281):

Displaying 8 items.

• Effect of disturbances at inlet on hypersonic boundary layer transition on a blunt cone at small angle of attack (Q605131) (← links)
• Effect of the cone nose bluntness and the ultrasonically absorptive coating on transition in a hypersonic boundary layer (Q665591) (← links)
• Quantifying the parameter dependent basin of the unsafe regime of asymmetric Lévy-noise-induced critical transitions (Q824060) (← links)
• Mechanism of transition in a hypersonic sharp cone boundary layer with zero angle of attack (Q940372) (← links)
• PSE as applied to problems of transition in compressible boundary layers (Q940667) (← links)
• Conservation relation of generalized growth rate in boundary layers (Q2313448) (← links)
• Direct numerical simulation of hypersonic boundary layer transition over a blunt cone with a small angle of attack (Q5305046) (← links)
• Toward an understanding of supersonic modes in boundary-layer transition for hypersonic flow over blunt cones (Q5745206) (← links)