Separation and reattachment near the leading edge of a thin oscillating airfoil

DOI10.1017/S0022112088000722zbMath0642.76076OpenAlexW2005312983MaRDI QIDQ3783736

Tuncer Cebeci, Suzanne M. Schimke, A. A. Khattab

Publication date: 1988

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/s0022112088000722

zbMATH Keywords

stagnation pointstability criterionseparated flowpressure distributionflow reversalnumerical errorsevolution of unsteady boundary layersinstability of separation bubblesthin oscillating airfoilunsteady boundary- layer equationsvicinity of the leading edge

Mathematics Subject Classification ID

Multiphase and multicomponent flows (76T99) Boundary-layer theory, separation and reattachment, higher-order effects (76D10) General aerodynamics and subsonic flows (76G25) Basic methods in fluid mechanics (76M99)

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Vortex-induced boundary-layer separation. Part 2. Unsteady interacting boundary-layer theory

Cites Work

• Unsteady separation
• The laminar boundary layer on a circular cylinder started impulsively from rest
• Computer extension and analytic continuation of Blasius’ expansion for impulsive flow past a circular cylinder
• Marginal Separation
• Accurate Difference Methods for Nonlinear Two-Point Boundary Value Problems