Pages that link to "Item:Q1925233"
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The following pages link to Analysis of the three-dimensional turbulent boundary layer on the surface of an arbitrary body at large angles of attack (Q1925233):
Displaying 4 items.
- Three-dimensional boundary layers on complex-shaped bodies at angles of attack (Q1359926) (← links)
- The effect of sweep-angle variation on the turbulence structure in a separated, three-dimensional flow (Q1405760) (← links)
- Effects of second-approximation of boundary layer theory in three-dimensional flow over bodies with a large aspect ratio at small angles of incidence (Q1925215) (← links)
- Triple-deck analysis of formation of supersonic and local separation regions in transonic steady flow over a roughness element on the surface of a body of revolution (Q2995711) (← links)