Fundamentals of Aerodynamics¶
Anderson, J. D. (2017). Fundamentals of Aerodynamics. McGraw-Hill.
Cited by¶
1 citation across 1 artifact.
Each citation links to the sentence it supports in the citing article.
Primes¶
- Edge Effect
- That steep gradient drives the non-linear local responses that decide the wing's behavior: viscous shear (hence skin-friction drag), the laminar-to-turbulent transition, and — the degrading contingency — flow separation and stall when the band cannot negotiate an adverse pressure gradient.
This sourceTreats boundary-layer separation and stall under adverse pressure gradients and design levers (transition control, vortex generators, suction) for managing the band.
- That steep gradient drives the non-linear local responses that decide the wing's behavior: viscous shear (hence skin-friction drag), the laminar-to-turbulent transition, and — the degrading contingency — flow separation and stall when the band cannot negotiate an adverse pressure gradient.
Verification¶
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Does it back the claim? Not recorded. The single citation of this work carries no recorded support check.
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Registry ID ref:b2c326cb068e · see in the full table