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acid airfoil angle applied approximately ASME axial Axial-Flow Axial-Flow Compressor blade row boiler boundary layer calculated capacity cascade cavitation cent coefficient constant corrosion curve cycle dashpot dead band deaerator determined diameter effect efficiency electrical engine enthalpy equation experimental factor feedwater feedwater heaters force frequency gear governor head heat rate heater impeller increase indicated inlet Mach number Kaplan turbines limit load low-pressure machine maximum measured mechanical method NACA RM normal NPSH obtained operation over-all oxygen paper performance plane strain pressure ratio pump radial reduced reheat relative rotor runaway speed shock losses shown in Fig shows silica specific speed stage static stator steam stress subsonic sulfur trioxide superheater supersonic surface Table tank temperature tion transonic compressor tube turbine unit valve variation velocity vibration weight flow welded weldments