Polynomial Chaos Expansion-Based Uncertainty Model for Fast Assessment of Gas Turbine Aero-Engines Thrust Regulation: A Sparse Regression Approach
Manufacturing tolerance uncertainties in gas turbine aero-engines are unavoidable, which
adversely influence the thrust control performance of newly produced aero-engines …
adversely influence the thrust control performance of newly produced aero-engines …
Polynomial Chaos Expansion-Based Uncertainty Model for Fast Assessment of Gas Turbine Aero-Engines Thrust Regulation: A Sparse Regression Approach
Uncertainties in gas turbine aero-engines are unavoidable among which manufacturing
tolerance is a typical manifestation. Uncertainties from manufacturing tolerance directly …
tolerance is a typical manifestation. Uncertainties from manufacturing tolerance directly …
Robustness Analysis on the Aerothermal Performance of Turbine Blade Squealer Tip
M Huang, Z Li, J Li - Journal of Engineering for Gas …, 2022 - asmedigitalcollection.asme.org
An improved efficient uncertainty quantification (UQ) analysis framework is proposed by the
combination of sparse polynomial chaos expansion (PCE) and universal Kriging (UK) …
combination of sparse polynomial chaos expansion (PCE) and universal Kriging (UK) …
A data-driven polynomial chaos method for uncertainty quantification of a subsonic compressor cascade with stagger angle errors
H Wang, L Gao, G Yang, B Wu - … Part A: Journal of Power and …, 2024 - journals.sagepub.com
The probability-based uncertainty quantification (UQ) methods require a large amount of
sampled data to construct the probability distribution of uncertain input parameters …
sampled data to construct the probability distribution of uncertain input parameters …
Investigations on the aerothermal performance of the turbine blade winglet squealer tip within an uncertainty framework
M Huang, Z Li, J Li - Aerospace Science and Technology, 2022 - Elsevier
A improved efficient uncertainty quantification analysis framework is proposed by the
combination of sparse Polynomial Chaos Expansion (PCE) and Universal Kriging (UK) …
combination of sparse Polynomial Chaos Expansion (PCE) and Universal Kriging (UK) …
Efficient uncertainty quantification and Sensitivity analysis on the Aerothermal performance of turbine blade Squealer tip
M Huang, Z Li, J Li, L Song - Journal of …, 2022 - asmedigitalcollection.asme.org
It is important to accurately estimate the impact of flow and geometric variations for
engineering design and manufacture. In this paper, an efficient uncertainty quantification …
engineering design and manufacture. In this paper, an efficient uncertainty quantification …
Uncertainty analysis of global and local performance impact of inflow and geometric uncertainties using sparse grid-based non-intrusive polynomial chaos
Z Guo, W Chu, H Zhang - … , Part A: Journal of Power and …, 2022 - journals.sagepub.com
Flow variations at the inlet boundary due to the compressor operational condition changes
and geometric variations of the realistic compressor blades due to the manufacturing …
and geometric variations of the realistic compressor blades due to the manufacturing …
Uncertainty quantification using generalized polynomial chaos for online simulations of automotive propulsion systems
Online simulations conducted in vehicles can enable predictive control of automotive
systems. This capability can be especially valuable for complex propulsion systems to …
systems. This capability can be especially valuable for complex propulsion systems to …
Uncertainty quantification of heat transfer for a highly loaded gas turbine blade endwall using polynomial chaos
P Zhu, Y Yan, L Song, J Li… - … Expo: Power for …, 2016 - asmedigitalcollection.asme.org
The durability of highly loaded gas turbine blade is significantly impacted by high heat
transfer. The heat transfer performance of the gas turbine endwall can be varied significantly …
transfer. The heat transfer performance of the gas turbine endwall can be varied significantly …
Aerothermal performance robustness and reliability analysis of turbine blade squealer tip with film cooling
M Huang, K Zhang, Z Li, J Li - Journal of …, 2024 - asmedigitalcollection.asme.org
The uncertainty quantification in the turbine components' aerodynamic and heat transfer
performances is widely considered to be the most challenging topic due to its intricate and …
performances is widely considered to be the most challenging topic due to its intricate and …