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Effect of a reduction in stator solidity on performance of a transonic turbine
Comparison of results of experimental and theoretical studies of blade-outlet boundary-layer characteristics of stator blade for a high subsonic Mach number turbine
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Published Year
1950-1959 (2) *
Subject
Aircraft gas-turbines--Blades (2) *
Aerodynamics, Transonic (1)
Boundary layer (1)
Gas-turbines--Performance (1)
Turbines--Blades--Aerodynamics (1)
Author
Hauser, Cavour H. (1)
Miser, James W. (1)
Nusbaum, William J. (1)
Stewart, Warner L. (1)
Wong, R. Y. (1)