Pages that link to "Item:Q404050"
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The following pages link to Linear evolution of controlled disturbances in the supersonic boundary layer on a swept wing (Q404050):
Displaying 4 items.
- Numerical investigation of evolution of disturbances in supersonic sharp cone boundary layers (Q944688) (← links)
- Experimental investigation of the development of secondary perturbations on a swept wing (Q1402858) (← links)
- Evolution of artificial perturbations in the boundary layer on a plate and in its wake at supersonic free-stream velocity (Q1403620) (← links)
- Linear modal instabilities around post-stall swept finite wings at low Reynolds numbers (Q5085110) (← links)