7 pages matching EPR and WCFAN in this book
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afterburner altitude approximately baseline engine CIVV component deviation parameter constraints control variables CPSM cruise conditions decrease in TSFC decreasing the FTIT DEEC DEHPT DELPT digital electronic DINL Dryden Flight Research DWFAN DWHPC dynamics engine and linear engine control engine operating condition engine parameters engine pressure ratio EPR and WCFAN fan turbine inlet Flight Research Facility function of Mach Gilyard HIDEC high-pressure compressor airflow high-pressure turbine Kalman filter lb/sec linear programming problem Mach number maintain FNP maximum thrust mode McDonnell Aircraft McDonnell Douglas Corporation MIL power minimum FTIT mode minimum fuel mode mode evaluation mode is designed NASA Dryden Flight nonlinear calculations optimization process output variables percent performance seeking control PLA of 40 propulsion system model PSC algorithm PSC engaged pulse code modulation RCVV SMHC SSVM subsonic thrust-specific fuel consumption tion TLER turbofan variables WF vector of control West Palm Beach