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airfoil area-weighted total pressure autocorrelation Axial distance bicone Circumferential configuration Accb Conical section correlation function coefficient cowl and centerbody critical inlet operation critical operation cross-correlations Cross-covariance Data Dccb denote static pressure diffuser exit total dynamic static pressure exit total pressure flow separated fluctuating component fluctuating pressures free-stream Mach number fuser H/p oijej H/p ouej hertz Joseph F Mach 2.0 centerbody mass-flow ratio mid-diffuser mixing NASA operating conditions operation at Mach overboard bypass system peak operating Px/pn recovery and distortion resulted sample random process sealed bypass Second cone set II vortex shown in figure Solid symbols denote static pressure distributions static pressure taps steady-state distortion struts Supersonic Wind Tunnel symbols denote critical symbols denote static terminal shock throat boundary layer total pressure probe total pressure profiles total pressure rakes total pressure recovery viscous layer vortex action Vortex generator set vortex generators installed wall dynamic static wall static pressure x/Rc