2004 · 29 citations · 11 references
EngineeringPhysicsAerodynamicsComputational Fluid DynamicsFluid DynamicsHypersonic AerodynamicsSubsonic Aerodynamics
Predictions of the flow over a wall-mounted hump are obtained using solutions of the Reynolds-averaged Navier-Stokes (RANS) equations and Detached-Eddy Simulation (DES). The upstream solution is characterized by a two-dimensional turbulent boundary layer with a thickness approximately half of the maximum hump thickness measured at a location about two chord lengths upstream of the leading edge. The Reynolds number based on the hump chord length is 9.75 × 10 5. A slot at approximately 65 % chord (C) is used for flow control via a spatially uniform (with respect to the spanwise coordinate) steady suction, and with alternating suction/blowing. Solutions of the two- and three-dimensional RANS equations are obtained using the Spalart-Allmaras and SST turbulence models. DES is applied to a three-dimensional geometry corresponding to an extruded section of the hump. DES predictions of the baseline case exhibit a threedimensional chaotic structure in the wake, with a mean reverse-flow region that is 20% shorter than predicted by the two-dimensional RANS computations. DES predictions of the pressure coefficient in the separated-flow region for the baseline case exhibit good agreement with measurements and are more accurate than either the S-A or SST RANS
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Two-equation eddy-viscosity turbulence models for engineering applications
Florian Menter · AIAA Journal · 1994 · 20.7K citations
Delay of airfoil stall by periodic excitation
Avi Seifert, Ahmad Darabi, I. Wyganski · Journal of Aircraft · 1996 · 634 citations