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Reduced Order Modeling of the Unsteady Pressure on Turbine Rotor Blades Using Deep Learning
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Abstract. In transonic turbine stages, complex interactions between the trailing edge shocks from nozzle guide vanes and the rotor blades generate unsteady wall pressure fields, affecting the rotor aerodynamic performance ...
Aerodynamic Optimization of the Low-Pressure Turbine Module: Exploiting Surrogate Models in a High-Dimensional Design Space
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Further improvement of state-of-the-art low-pressure (LP) turbines (LPTs) has become progressively more challenging. LP design is more than ever confronted to the need to further integrate complex models and to shift from ...
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