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RISThe Effect of Rotor Tip Clearance Size onto the Separated Flow Through a Super-Aggressive S-Shaped Intermediate Turbine Duct Downstream of a Transonic Turbine Stage
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The demand for a further increased bypass ratio of aero engines will lead to low pressure turbines with larger diameters, which rotate at a lower speed. Therefore, it is necessary to guide ...
Shorten the Intermediate Turbine Duct Length by Applying an Integrated Concept
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The demand of further increased bypass ratio of aero engines will lead to low pressure turbines with larger diameters, which rotate at lower speed. Therefore, it is necessary to guide the ...