Sensitivity analysis and modeling uncertainties quantification for impinging-film cooling via active subspaces
• Interaction effect of coolant and hot mainstream on impinging-film cooling under three interaction modes TF, TBL and WJ are quantitatively evaluated via active subspace. • 1-D active subspaces are sufficient to map cooling effectiveness in TF and TBL modes while multi-dimensional ones are warranted for WJ mode. • Cooling effectiveness is the most sensitive to blowing ratio and turbulent effects are more significant in near fields for TF and TBL modes. • Twofold impacts of blowing ratio and turbulence on cooling are identified in WJ mode by the “parabolic law” of cooling effectiveness versus active variables. • Propagations of input uncertainties to cooling effectiveness are space- and operational condition-dependent. Within the context of exploiting efficient cooling methods for advanced gas turbine combustors, understanding the fundamental physics for impinging-film cooling under various operational conditions is of significance. In this paper, impacts of different interaction modes between coolant and hot mainstream on the impinging-film cooling are quantitatively evaluated via active subspace (AS) method. Three interaction modes are considered, i.e., a transitional flow (TF), a turbulent boundary layer (TBL) and a wall jet (WJ). Sensitivities and uncertainties of cooling effectiveness η with respect to coolant mass flow rate M c and model parameters ( C μ , C ε 1 , C ε 2 , P r tw ) are estimated. Results show that 1-D active subspaces are sufficient to map η in TF and TBL modes while high-dimensional active subspaces are warranted for WJ mode, indicating its more complicated interaction between cold and hot flows. η is the most sensitive to and dominated by M c especially in the slot and far fields, and turbulent effects are more significant in the near field than other places. Specifically, an increase in M c or a decrease in turbulent level monotonously improves η in TF and TBL modes while initially increases η then reduces it for WJ mode. Further analysis of flow characteristics of WJ mode demonstrates that the reduction in η results from the strengthened impingement-induced streamwise vortexes and thereby, enhanced mixing between the coolant and mainstream. The propagation of the input uncertainty to η is space- and operational condition-dependent, consistent with the evolution of active subspaces.
Authors
- Jingyu Zhang (ORCID: https://orcid.org/0000-0002-3777-1509)
- Jieli Wei (ORCID: https://orcid.org/0000-0001-6705-9937)
- Nana Wang (ORCID: https://orcid.org/0000-0002-6896-0038)
- Xiaomin He (ORCID: https://orcid.org/0000-0003-3305-5449)
Institutions
- Nanjing University of Aeronautics and Astronautics (CN)
Publication Details
- Journal
- International Journal of Heat and Mass Transfer
- Published
- 2025-04-05
- DOI
- https://doi.org/10.1016/j.ijheatmasstransfer.2025.127046
- Citations
- 3
- Primary Topic
- Heat Transfer Mechanisms
- Type
- article
- Field-Weighted Citation Impact
- 2.14