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searching for Adverse pressure gradient 8 found (15 total)

alternate case: adverse pressure gradient

Dean number (1,424 words) [view diff] exact match in snippet view article find links to article

wall and forms an asymmetric velocity profile. There will be an adverse pressure gradient generated from the curvature with an increase in pressure, therefore

Boundary layer control (1,212 words) [view diff] exact match in snippet view article find links to article

control the boundary layer separation that occurs due to the adverse pressure gradient. Rotation of the cylinder can reduce or eliminate the boundary

Supercritical airfoil (2,107 words) [view diff] exact match in snippet view article find links to article

condition. However, if AOA is increased to the stalling point, an adverse pressure gradient builds, and a shockwave can form within the thin boundary layer

Skin friction drag (1,881 words) [view diff] exact match in snippet view article find links to article

reduction of skin friction by riblets under the influence of an adverse pressure gradient". Experiments in Fluids. 15 (1): 17–26. Bibcode:1993ExFl...15

Surfboard fin (3,562 words) [view diff] exact match in snippet view article find links to article

speeds, the turbulent boundary layer helps the flow overcome an adverse pressure gradient and allows the fin to remain attached to the surface longer than

Falkner–Skan boundary layer (2,345 words) [view diff] exact match in snippet view article find links to article

problem reduces to the Hiemenz flow. Here, m < 0 corresponds to an adverse pressure gradient (often resulting in boundary layer separation) while m > 0 represents

Couette flow (3,138 words) [view diff] exact match in snippet view article find links to article

(h-y)+U{\frac {y}{h}}.} The pressure gradient can be positive (adverse pressure gradient) or negative (favorable pressure gradient). In the limiting case

Swept wing (8,240 words) [view diff] exact match in snippet view article find links to article

conditions around the rest of the aircraft, and as the flow enters an adverse pressure gradient in the aft section of the wing, a discontinuity emerges in the