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Experiments of effects of inlet-air distortion on aerodynamic performance in transonic
plugboard simulator inlet-air distortion transonic axial-flow compressor shock wave disturbance
2014/5/19
The inlet-air distortion which was caused by high angle-of-attack flight was simulated by plugboard.Experiments were conducted on a transonic axial-flow compressor's rotor at 98% rotating speed.The fl...