Search
Now showing items 1-1 of 1
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 ...
CSV
RIS