Application of Engineering Transition Models to an Isolated Helicopter Rotor in Hovering Flight
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Ning Qin | Jason Hill | Scott Shaw | N. Qin | S. Shaw | Jason Hill
[1] D. Wilcox. Simulation of Transition with a Two-Equation Turbulence Model , 1994 .
[2] Max F. Platzer,et al. Analysis of low Reynolds number airfoil flows , 1994 .
[3] Tuncer Cebeci,et al. Essential ingredients of a method for low Reynolds-number airfoils , 1989 .
[4] P. F. Yaggy,et al. Experimental Boundary Layer Study on Hovering Rotors , 1966 .
[5] B. Thwaites,et al. Approximate Calculation of the Laminar Boundary Layer , 1949 .
[6] H. Stock,et al. Airfoil Validation Using Coupled Navier-Stokes and e Transition Prediction Methods , 2002 .
[7] Ning Qin,et al. A matrix-free preconditioned Newton/GMRES method for unsteady Navier-Stokes solutions , 2000 .
[8] Andreas Krumbein,et al. Transitional Flow Modeling and Application to High-Lift Multi-Element Airfoil Configurations , 2003 .
[9] G. J. Walker. Transitional Flow on Axial Turbomachine Blading , 1987 .