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- W229652767 abstract "Report presenting efficiency tests on a single-stage gas turbine with an 11.0-inch pitch-line diameter wheel and a nozzle diaphragm with cast airfoil-shaped nozzle blades using atmospheric air as the driving fluid. A comparison is made with the same turbine but with different nozzle blades. Results regarding the efficiency curves and further information about velocity effects are provided." @default.
- W229652767 created "2016-06-24" @default.
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- W229652767 date "1945-09-01" @default.
- W229652767 modified "2023-09-26" @default.
- W229652767 title "The Performance of a Single-Stage Impulse Turbine Having an 11.0-Inch Pitch-Line Diameter Wheel with Cast Airfoil-Shaped and Bent Sheet-Metal Nozzle Blades" @default.
- W229652767 hasPublicationYear "1945" @default.
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