Numerical investigation of the unsteady effect on the onset of leading-edge separation in dynamic stall.
Numerical experiments are conducted to simulate airfoils pitching up at constant rates into the dynamic stall regime using the Beam and Warming algorithm for compressible Navier-Stokes equations. The Bladwin and Lomax algebraic turbulence model is used to mimic turbulent flow downstream of a point d...
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| Language: | en |
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The University of Arizona.
1993
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| Online Access: | http://hdl.handle.net/10150/186411 |