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OffDesign Conditions and OffDesign Performance
Aerodynamic Characteristics for the Computing Proce
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acceleration ambient angle of attack apparatus axial axial compressor blade bleed flow bleed location boundary points calculation method calculation procedure calculation specifications components COMPRESSOR BLEED compressor efficiency compressor inlet compressor map compressor performance compressor set computer program constant cooling curve cycle decrease design conditions determined disc effects engine enthalpy exhaust temperature figure flow angle flow circuit flow coefficient flow equation fuel flow gas turbine plant geometry given high speed influence inlet flow inlet guide vane inlet pressure inlet stages input data intake isentropic ISO Conditions labyrinth seal low speed mass flow rate maximum non-return flap nozzle obtained off-design operation parameters percent speed polytropic power output power plant pressure losses pressure ratio rotating stall rotor scheme shows shrink fit slope speed range stage bleed Stagnation Pressure starting suction throttle torque turbine inlet temperature turbine stage values valve variable inlet guide variation velocity