Novel method predicts turbine performance using small sample data, indicating significant accuracy improvements.
The turbine, as a critical component of gas turbines, has been widely used in marine propulsion. However, under small-sample data conditions, it is confronted with many challenges like calibration difficulties and over-fitting. To address these issues, a rapid performance prediction method based on loss model theory and small-sample data-driven adaptive calibration was proposed. Various energy loss models were integrated and the optimal model was identified through systematic multi-criteria evaluation. Key parameters were determined using Self-Organizing Map analysis for intelligent dimensionality reduction. This process identified the most sensitive coefficients, which reduced the number of parameters from 29 to 8 and cut calibration time by 50%. For the single-stage turbine, the maximum prediction error was reduced from 3.84% to 0.83%. High accuracy was maintained in multi-stage turbines, where inherent overestimation of losses was effectively corrected as validated by 3D flow details. Practical value was demonstrated by embedding the model into a zero-dimensional dynamic simulation with a maximum relative error of 1.0%. This research supports the construction and optimization of digital models for gas turbines.
No takes yet. Share an insight, caveat, or question.
Zheng et al. (2026) studied this question.
Synapse has enriched 5 closely related papers on similar clinical questions. Consider them for comparative context: