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Experimental Investigation of a High Subsonic Mach Number Turbine Having High Rotor Blade Suction-Surface Diffusion

Comparison of results of experimental and theoretical studies of blade-outlet boundary-layer characteristics of stator blade for a high subsonic Mach number turbine

Experimental Investigation of a High Subsonic Mach Number Turbine Having a 40-Blade Rotor With Zero Suction-Surface Diffusion

Published Year

• 1950-1959 (3)

Subject

• Aircraft gas-turbines--Blades (1)
• Boundary layer (1)
• Turbines--Blades--Aerodynamics (1)

Author

• Nusbaum, William J. (3) *
• Hauser, Cavour H. (1)
• Wasserbauer, Charles A. (1)

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