Performance of Vortex Generators in a Mach 2.5 Low-bleed Full-scale 45-percent-internal-contraction Axisymmetric Inlet |
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6.0 Axial distance airfoil area-weighted total pressure Autocorrelation bicone bleed slot boundary layer rake centerbody bleed flow Centerbody throat boundary configuration Accb Conical section correlation function coefficient cowl and centerbody critical inlet operation critical operation cross-correlations Dccb denote static pressure Diffuser exit rakes diffuser exit total dynamic static pressure exit total pressure flow separated fluctuating component fluctuating pressures free-stream Mach number fuser hertz Mach 2.0 centerbody mass-flow ratio Mid-diffuser rake mixing operation at Mach overboard bypass system Pitot pressure recovery pressure contours Pressure transducer Px/Po Rake 1 Rake Rake 12 recovery and distortion sealed bypass set II vortex shown in figure Solid symbols denote static pressure 1.0 struts super sonic Supersonic symbols denote static terminal shock throat boundary layer Throat exit rakes top quadrant Total pressure profiles total pressure recovery viscous layer vortex action Vortex generator set vortex generators installed wall dynamic static wall static pressure x/R r/R x/R x/Rc