Pages that link to "Item:Q5948593"
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The following pages link to Assessment of numerical uncertainty around shocks and corners on blunt trailing-edge supercritical airfoils (Q5948593):
Displaying 3 items.
- URANS computations of shock-induced oscillations over 2D rigid airfoils: influence of test section geometry (Q608064) (← links)
- Grid refinement study for three dimensional CFD model involving incompressible free surface flow and rotating object (Q1648127) (← links)
- Numerical uncertainties in transonic flow calculations for aerofoils with blunt trailing edges (Q4359266) (← links)