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Article

Wind Tunnel Process Mach Number Prediction Based on Modal, Stage, and Intra-Stages Three-Layer Partitioning

1
Harbin Institute of Technology Shenzhen, School of Science, Shenzhen 518000, China
2
Aviation Technology Key Laboratory of Aerodynamics Research in High-Speed and High Reynolds, Shenyang 110819, China
3
Aerodynamics Research Institute, Aviation Industry Corporation of China (AVIC), Shenyang 110819, China
4
High Velocity Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
5
College of Information Science and Engineering, Northeastern University, Shenyang 110819, China
*
Author to whom correspondence should be addressed.
Aerospace 2025, 12(5), 439; https://doi.org/10.3390/aerospace12050439
Submission received: 3 March 2025 / Revised: 17 April 2025 / Accepted: 12 May 2025 / Published: 15 May 2025

Abstract

The wind tunnel experiment process is a nonlinear process with complex process characteristics. It is the primary task to master the key physical parameters and performance evaluation criteria during its operation. Aiming at the characteristics of multi-mode, multi-stage and intra-stage changes in the wind tunnel process, this paper proposes a Mach number prediction method based on mode, stage and intra-stage division. Firstly, mode division is carried out. The K-means clustering method is mainly used to cluster process data. The elbow rule is used to determine the cluster number K. The Mach number is used as the index variable to divide the process into phases, and divide the phases into stable parts and transitional parts according to different process characteristics. Considering the nonlinearity of the data, a kernel partial least squares prediction model is constructed for the stable process. Considering the dynamic characteristics of data, a dynamic partial least squares prediction model is constructed for the transitional process. The proposed method has been applied to multi-stage nonlinear wind tunnel experiments, and satisfactory results have been obtained.
Keywords: wind tunnel; Mach number; multi-mode; multi-stage; intra-stage wind tunnel; Mach number; multi-mode; multi-stage; intra-stage

Share and Cite

MDPI and ACS Style

Yuan, H.; Guo, J.; Yu, W.; Zhao, L. Wind Tunnel Process Mach Number Prediction Based on Modal, Stage, and Intra-Stages Three-Layer Partitioning. Aerospace 2025, 12, 439. https://doi.org/10.3390/aerospace12050439

AMA Style

Yuan H, Guo J, Yu W, Zhao L. Wind Tunnel Process Mach Number Prediction Based on Modal, Stage, and Intra-Stages Three-Layer Partitioning. Aerospace. 2025; 12(5):439. https://doi.org/10.3390/aerospace12050439

Chicago/Turabian Style

Yuan, Haixuan, Jin Guo, Wenshan Yu, and Luping Zhao. 2025. "Wind Tunnel Process Mach Number Prediction Based on Modal, Stage, and Intra-Stages Three-Layer Partitioning" Aerospace 12, no. 5: 439. https://doi.org/10.3390/aerospace12050439

APA Style

Yuan, H., Guo, J., Yu, W., & Zhao, L. (2025). Wind Tunnel Process Mach Number Prediction Based on Modal, Stage, and Intra-Stages Three-Layer Partitioning. Aerospace, 12(5), 439. https://doi.org/10.3390/aerospace12050439

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