Pages that link to "Item:Q431895"
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The following pages link to An experimental investigation of the separated-flow transition under high-lift turbine blade pressure gradients (Q431895):
Displaying 6 items.
- An experimental investigation of the separated-flow transition under high-lift turbine blade pressure gradients (Q431895) (← links)
- Application of a synthetic jet to control boundary layer separation under ultra-high-lift turbine pressure distribution (Q652305) (← links)
- Experimental investigation of turbulence influence of wake passing on the boundary layer development of highly loaded turbine cascade blades (Q1417658) (← links)
- Effects of freestream turbulence on separated boundary layer in a low-Re high-lift LP turbine blade (Q1645568) (← links)
- Improved understanding of two-phase flow phenomena based on unsteady blade pressure measurements (Q2770626) (← links)
- Response of a laminar separation bubble to impulsive forcing (Q5364746) (← links)
