An improved steady inverse method for turbomachinery aerodynamic design
Author:
Affiliation:
1. School of Energy and Power Engineering, Dalian University of Technology, Dalian, China
2. School of Power and Energy, Northwestern Polytechnical University, Xi’an, China
Funder
National Natural Science Foundation of China
National Program on Key Basic Research Project
Publisher
Informa UK Limited
Subject
Applied Mathematics,Computer Science Applications,General Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/17415977.2016.1178259
Reference21 articles.
1. Inverse method for turbomachine blades using shock-capturing techniques
2. Euler-based inverse method for turbomachine blades. I - Two-dimensional cascades
3. Euler-Based Inverse Method for Turbomachine Blades, Part 2: Three-Dimensional Flows
4. Improving Aerodynamic Matching of Axial Compressor Blading Using a Three-Dimensional Multistage Inverse Design Method
5. Three-dimensional viscous inverse method for axial blade design
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