Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane
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107 Solid symbols afterburner Ames Research Center Angle of attack angle PT2AVG KA2 corrected engine airflow denote last points Distortion D KA2 distortion descriptor distortion fac distortion factor DTMM distortion factor KA2 Dryden Flight Research DTMM distortion factor engine face engine hub engine serial number engine stall engine-face total pressure Evaluation F-15 aircraft F-15 Airplane F100 engine factor K6 fan distortion factor Figure Flight Research Facility Flight test inlet guide vanes inlet third ramp KA2 KQ KRA2 Karen G kPa psia KQ KRA2 DTMM KRA2 DTMM WAC Mach number measurement N/m2d 6 psid NASA percent points before engine pressure to static PS2 probe PT2AVG KA2 KQ PT2AVG/PTINF PT2MAX radial distortion factor ramp angle fig Ramp angle PT2AVG ramp excursions RAMP3L Run WAC serial number P680059 Solid symbols denote Static Pressure Probe sure at engine symbols denote last third ramp angle tion tortion total pressure probes turbofan value of total