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Aerodynamic Optimization of High Pressure Turbines for Lean Burn Combustion System
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Modern leanburn combustors make use of high flow swirl to maintain flame stability. The swirling flow can persist downstream of the turbine first vane, changing the loading on the rotor, leading to a reduction in efficiency. ...
Automatic Design Optimization of Profiled Endwalls Including Real Geometrical Effects to Minimize Turbine Secondary Flows
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper presents a novel optimization methodology based on both adjoint sensitivity analysis and trust-based dynamic response surface modeling to improve the performance of a modern turbine of a large civil aero-engine ...