An efficient sparse surrogate model for aerodynamic characteristics of a supersonic compressor cascade with uncertain geometric deformations

This publication has 27 references indexed in Scilit:

• A dimensionality reduction method for uncertainty study of geometric variations of turbomachinery blades
  Aerospace Science and Technology, 2024
• Uncertainty quantification study of the aerodynamic performance of high-altitude propellers
  Aerospace Science and Technology, 2023
• A data-driven non-intrusive polynomial chaos for performance impact of high subsonic compressor cascades with stagger angle and profile errors
  Aerospace Science and Technology, 2022
• Investigations on the aerothermal performance of the turbine blade winglet squealer tip within an uncertainty framework
  Aerospace Science and Technology, 2022
• Nonlinear uncertainty quantification of the impact of geometric variability on compressor performance using an adjoint method
  Chinese Journal of Aeronautics, 2022
• Performance impact of flow and geometric variations for a turbine blade using an adaptive NIPC method
  Aerospace Science and Technology, 2019
• Statistical evaluation of performance impact of manufacturing variability by an adjoint method
  Aerospace Science and Technology, 2018
• Sparse grid-based polynomial chaos expansion for aerodynamics of an airfoil with uncertainties
  Chinese Journal of Aeronautics, 2018
• Adjoint aerodynamic optimization of a transonic fan rotor blade with a localized two-level mesh deformation method
  Aerospace Science and Technology, 2018
• Multivariate function approximations using the D-MORPH algorithm
  Applied Mathematical Modelling, 2015