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aerodynamic aftermixed critical velocity aftermixed flow angle annular cascade axial chord based on kinetic bellmouth Blade calculated cascade facility centimeter CHANEL program TSONIC combination probe Combination survey probe computer program conservation of mass critical velocity ratio described in reference design critical velocity design value downstream end wall boundary End wall total exit flow angle exit section FORTRAN hub and tip ideal aftermixed critical incidence angles Lewis Research Center mean radius mean section NASA TM obtained overall aftermixed efficiency program TSONIC program réf secondary flow losses shown in figure solid vanes static pressure suction surface surface critical velocity surface static-pressure survey data survey measurements survey plane station test section test vanes theoretical results tip wall total pressure probe TSONIC program Experimental Turbomachine V/Vcr vane efficiency Vane exit vane height vane inlet vane passage vane performance vane surface critical vane trailing edge Variation of aftermixed vortex core wall boundary layers wall total pressure