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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
Author:
Gabriel, David S.
Year:
1945
Document Type:
N/A
Series:
NACA Wartime Reports
Report Number:
NACA-WR-E-233, NACA-ARR-E5H31
Link:
https://digital.library.unt.edu/ark:/67531/metadc61856/
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