论文信息 - A Fast Method for the Prediction of Dynamic Stall Onset on Turbomachinery Blades - 字舞流文

A Fast Method for the Prediction of Dynamic Stall Onset on Turbomachinery Blades

ASME Paper No. 97-GT-101, presented at the 1997 ASME/IGTI Turbo Expo., Orlando, Florida, June 1997.

Max F. Platzer | Kevin D. Jones | M. Platzer | K. D. Jones

[1] Max F. Platzer,et al. Numerical Investigation of Stall Flutter , 1994 .

[2] G. Hancock,et al. The unsteady motion of a two-dimensional aerofoil in incompressible inviscid flow , 1978, Journal of Fluid Mechanics.

[3] Max F. Platzer,et al. Wake Structures Behind Plunging Airfoils: A Comparison of Numerical and Experimental Results , 1996 .

[4] J. Hess,et al. Calculation of potential flow about arbitrary bodies , 1967 .

[5] Miguel R. Visbal,et al. On the formation and control of the dynamic stall vortex on a pitching airfoil , 1991 .

[6] Peter J. Riester. A computational and experimental investigation of incompressible oscillatory airfoil flow and flutter problems. , 1993 .

[7] Max F. Platzer,et al. An Inviscid-Viscous Interaction Approach to the Calculation of Dynamic Stall Initiation on Airfoils , 1993 .