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100 percent 280 Relative circumferential analytical model attenuate fairly uniformly average mean total average tip static Braithwaite centi Circumferential profiles Claude clean and distorted clean inlet clockwise compressor inlet counterclockwise deBogdan design rotor speed distorted and clean distorted area distorted inlet conditions distortion amplitude distortion at station high circumferential resolution inlet distortion inlet guide vane Inlet Pressure Distortion inlet-total-pressure distortion J85-13 turbojet engine Lewis Research Center located maximum amplitude mean total pressure mean zone Mehalic MULTISTAGE COMPRESSOR NASA TM overall and stagewise percent of design percent of rotor Percent speed plots position of distorted pressure and temperature rake reached a maximum Relative circumferential position rise per stage rotor design speed screen trailing edge sinusoidal square wave Stage by stage stagewise compressor performances Static-pressure distortion station 2.0 stator temperature distortion throughout the compressor tip static pressure tip zone tortion total-pressure distortion total-pressure rise total-temperature distortion TT Tip Mean zero at stage