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  • Inlet Distortion and Blade Vibration in Turbomachines

    TANIDA Yoshimichi , NAGASHIMA Toshio

    Nonuniformity of inlet flows through a test compressor stage has been studied based upon 3-D semi-actuator disk theory. The results show that the rotor blade vibration greatly influences the attenuati …

    ISAS report 46(3), 93-103, 1981-02

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