TRANSONIC COMPRESSOR ROTOR CASCADE WITH BOUNDARY-LAYER SEPARATION: EXPERIMENTAL AND THEORETICAL RESULTS
暂无分享,去创建一个
[1] H. Starken,et al. Experimental cascade analysis of a transonic compressor rotor blade section , 1984 .
[2] P. Janssens,et al. A Viscid Inviscid Interaction Procedure for Two Dimensional Cascades , 1983 .
[3] D. E. Hobbs,et al. Inviscid-Viscous Interaction Analysis of Compressor Cascade Performance , 1990 .
[4] E. Elsholz,et al. Viscid-Inviscid Interaction Analysis on Airfoils with an Inverse Boundary Layer Approach , 1982 .
[5] H. Starken,et al. Inlet flow angle determination of transonic compressor cascades , 1992 .
[6] J. E. Carter,et al. A new boundary-layer inviscid iteration technique for separated flow , 1979 .
[7] J. D. Denton,et al. An Improved Time-Marching Method for Turbomachinery Flow Calculation , 1983 .
[8] H. Starken,et al. Theoretical and Experimental Analysis of a Compressor Cascade at Supercritical Flow Conditions , 1987 .
[9] A. Walz,et al. Boundary layers of flow and temperature , 1969 .