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The Effect of Inlet Temperature and Pressure on the Efficiency of Single-Stage Impulse Turbine Having a 13.2-Inch Pitch-Line Diameter Wheel
Author:
Chanes, Ernest R.
Year:
1945
Document Type:
N/A
Series:
NACA Wartime Reports
Report Number:
NACA-WR-E-232, NACA-ARR-E5H10
Link:
https://digital.library.unt.edu/ark:/67531/metadc61853/
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