The Impact of Forward Swept Rotors on Tip Clearance Flows in Subsonic Axial Compressors
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[1] N. Yamaguchi,et al. IGTC-8 Secondary-Loss Reduction by Forward-Skewing of Axial Compressor Rotor Blading(Session A-4 CASCADE PERFORMANCE) , 1991 .
[2] Aspi Rustom Wadia,et al. Inner Workings of Aerodynamic Sweep , 1997 .
[3] B. T. Sirakov,et al. Effect of Upstream Unsteady Flow Conditions on Rotor Tip Leakage Flow , 2002 .
[4] Aspi Rustom Wadia,et al. Forward Swept Rotor Studies in Multistage Fans With Inlet Distortion , 2002 .
[5] Frank E. Marble,et al. Endwall Blockage in Axial Compressors , 1999 .
[6] Nicholas A. Cumpsty,et al. The Use of Sweep and Dihedral in Multistage Axial Flow Compressor Blading—Part I: University Research and Methods Development , 2002 .
[7] Edward M. Greitzer,et al. The Role of Tip Clearance in High-Speed Fan Stall , 1991 .
[8] Masato Furukawa,et al. Controlled-Endwall-Flow Blading for Multistage Axial Compressor Rotor , 1997 .
[9] D. C. Wisler,et al. Loss Reduction in Axial-Flow Compressors Through Low-Speed Model Testing , 1985 .
[10] Nicholas A. Cumpsty,et al. The use of sweep and dihedral in multistage axial flow compressor blading-Part II: Low and high-speed designs and test verification , 2002 .
[11] Christopher B. Lorence,et al. Three Dimensional Linearized Navier-Stokes Calculations for Flutter and Forced Response , 1998 .
[12] Leroy H. Smith,et al. Sweep and Dihedral Effects in Axial-Flow Turbomachinery , 1963 .
[13] C. C. Koch,et al. Loss Sources and Magnitudes in Axial-Flow Compressors , 1976 .
[14] C. C. Koch,et al. Stalling Pressure Rise Capability of Axial Flow Compressor Stages , 1981 .