Upgrade and development of elastic surface inverse design method for axial compressor cascade with sharp-edged blades
Author:
Affiliation:
1. Mechanical Engineering Group, Pardis College, Isfahan University of Technology, Isfahan, Iran;
2. Department of Mechanical Engineering, Isfahan University of Technology, Isfahan, Iran
Publisher
Informa UK Limited
Subject
Computer Science Applications,Mechanics of Materials,Condensed Matter Physics,Modelling and Simulation,Numerical Analysis
Link
https://www.tandfonline.com/doi/pdf/10.1080/10407790.2019.1667680
Reference29 articles.
1. Inverse design of transonic airfoils using genetic algorithm and a new parametric shape method
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3. DIRECT DESIGN OF AIRFOIL SHAPE WITH A PRESCRIBED SURFACE PRESSURE
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