Technical Papers
Feb 5, 2024

Multistage Compressor Design Based on Dimensional Zooming

Publication: Journal of Aerospace Engineering
Volume 37, Issue 3

Abstract

This paper proposed an axial multistage compressor aerodynamic design methodology based on dimensional zooming. Two-dimensional design parameters are acquired through the dimensionality reduction of three-dimensional data to avoid dependence on the empirical loss models. The research on the zooming design method is conducted on a self-designed five-stage compressor. The method has considered the three-dimensional end wall viscosity loss and modified the blade profiles and blade stacking. It provided a path on how to improve the blade design based on computational fluid dynamics analysis. The aerodynamic performance, compressor characteristics of the prototype, and the zooming design are investigated and compared. The results show that the zooming design compressor performances are improved than those of the prototype one.

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Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.

Acknowledgments

The authors wish to thank the financial support of the National Natural Science Foundation of China joint fund for regional innovation and development U20A20298 and National Science and Technology Major Project 2017-II-0006-0019 and 2017-II-0009-0010.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 37Issue 3May 2024

History

Received: Aug 30, 2022
Accepted: Nov 29, 2023
Published online: Feb 5, 2024
Published in print: May 1, 2024
Discussion open until: Jul 5, 2024

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Ph.D. Candidate, College of Power and Energy Engineering, Harbin Engineering Univ., Harbin 150001, China. Email: [email protected]
Professor, College of Power and Energy Engineering, Harbin Engineering Univ., Harbin 150001, China. Email: [email protected]
Associate Professor, College of Power and Energy Engineering, Harbin Engineering Univ., Harbin 150001, China (corresponding author). Email: [email protected]

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