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On the Unsteady Supersonic Cascade With a Subsonic Leadin
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G P ESCHENBRENNER
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addition analysis angle application approximately ASME assumed bearing blade boiler boundary layer calculated cascade circulator coefficient combustion combustor components compressor considered constant deg F determined direction distribution drop droplet effect efficiency emission energy engine equation evaporator experimental factor failure flame flow fluid frequency fuel function gas turbine geometry given heat transfer important increase indicated inlet jet pump leading length lignite limit load loss Mach mean measured MECHANICAL method million nozzle obtained occur operating parameters particle percent performance period plant possible predicted presented pressure primary problem range ratio reactor reduced reference region relative rotor shown in Fig shows sodium solution speed stability stage steam suction surface Table temperature tion tons tube unit values velocity wall zone