Aerodynamic evaluation of two-stage axial flow turbine designed for Brayton-cycle space power system
Experimental design and performance test of two-stage axial-flow turbine designed for Brayton-cycle space power system
Engineering topics
Publications and source records attributed to Kofskey, M. G..
Experimental design and performance test of two-stage axial-flow turbine designed for Brayton-cycle space power system
Performance of two-stage axial flow turbine operating at different rotor tip clearance
Brayton cycle alternator drive turbine aerodynamics
Aerodynamic characteristics of two stage turbine for alternator drive in two shaft Brayton cycle space power system, measuring efficiency variations
NASA radial flow turbine research related to Brayton cycle power generator, investigating size, Reynolds number and speed effects on efficiency and flow
Radial flow turbines as related to Brayton cycle space power systems
Radial-inflow turbine performance over range of specific speeds
Cold performance characteristics of small radial inflow turbine designed for Brayton cycle power system
Cold argon and air performance of 6.02 inch radial inflow turbine designed for 10 kilowatt shaft output Brayton cycle space power generation system
Secondary-flow phenomena in stator and rotor-blade rows and their effect on turbine performance
Efficiency evaluation of two-stage turbine with low ratio of blade to jet speed suitable for bleed-type high energy liquid rocket applications