Efficient prediction of transonic flutter boundaries for varying Mach number and angle of attack via LSTM network
Wencheng Li, Xiumin Gao, Haojie Liu
Topics & Concepts
TransonicMach numberAirfoilAerodynamicsAeroelasticityComputational fluid dynamicsFlutterAngle of attackControl theory (sociology)Computer scienceSupersonic speedAerospace engineeringEngineeringArtificial intelligenceControl (management)Model Reduction and Neural NetworksAerodynamics and Fluid Dynamics ResearchFluid Dynamics and Turbulent Flows