Pages that link to "Item:Q761304"
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The following pages link to Influence of boundary layer on unsteady aerodynamic characteristics of blunt cones in a supersonic flow (Q761304):
Displaying 5 items.
- Effect of disturbances at inlet on hypersonic boundary layer transition on a blunt cone at small angle of attack (Q605131) (← links)
- Influence of blowing into the boundary layer on supersonic flow past an oscillating cone (Q799199) (← links)
- Effects of blunt trailing edge flow discharge in supersonic regime (Q1643607) (← links)
- Unsteadiness boundaries in supersonic flow over double cones (Q3389420) (← links)
- Characterization of instability mechanisms on sharp and blunt slender cones at Mach 6 (Q5034698) (← links)