Pages that link to "Item:Q1020441"
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The following pages link to Acoustic receptivity of Mach 4.5 boundary layer with leading-edge bluntness (Q1020441):
Displaying 4 items.
- 3D global optimal forcing and response of the supersonic boundary layer (Q2222579) (← links)
- Boundary-layer leading-edge receptivity to sound at incidence angles. (Q2755426) (← links)
- Sensitivity analysis of the aeroacoustic response of turbomachinery blade rows (Q4395996) (← links)
- Transition mechanisms in cross-flow-dominated hypersonic flows with free-stream acoustic noise (Q5112718) (← links)