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机译:上游尾流定相对跨音速轴向压气机性能的影响
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Department of Aeronautics and Astronautics, Gas Turbine Laboratory, MIT, Cambridge, MA 02139;
Department of Aeronautics and Astronautics, Gas Turbine Laboratory, MIT, Cambridge, MA 02139;
Department of Aeronautics and Astronautics, Gas Turbine Laboratory, MIT, Cambridge, MA 02139;
Department of Aeronautics and Astronautics, Gas Turbine Laboratory, MIT, Cambridge, MA 02139;
Department of Mechanical Engineering, Brigham Young University, Provo, UT 84602;
a: area; b_3: nondimensional wake phasing parameter; c_p: static pressure rise coefficient; f_0: tangential blade force per unit inlet flow area; h: boundary layer shape factor; et al;
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