Hypersonic inlet flow field reconstruction dominated by shock wave and boundary layer based on small sample physics-informed neural networks
Mingming Guo, Xue Deng, Yue Ma, Ye Tian, Jialing Le, Hua Zhang
Topics & Concepts
Hypersonic speedBoundary layerShock waveField (mathematics)Sample (material)InletArtificial neural networkAerospace engineeringMechanicsFlow (mathematics)Shock (circulatory)PhysicsBoundary (topology)Computer scienceEngineeringMechanical engineeringMathematical analysisMathematicsArtificial intelligencePure mathematicsMedicineThermodynamicsInternal medicineModel Reduction and Neural NetworksNuclear Engineering Thermal-HydraulicsFluid Dynamics and Turbulent Flows