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Publications by Aleksandr Sebelev
Effects of Hub Endwall Geometry and Rotor Leading Edge Shape on Performance of Supersonic Axial Impulse Turbine. Part I
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The Effect of Axial Velocity Ratio, Turbulence Intensity, Incidence and Leading Edge Geometry on the Off-Design Performance of a Turbine Blade Cascade.
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Experimental and Numerical Studies on Leading Edge Film Cooling Performance: Effects of Hole Exit Shape and Freestream Turbulence
Experimental Investigations on Effects of Axial Clearance on High-Speed Turbine Expansion Generator Rotor Response
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