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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

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)

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