Aerodynamic Inverse Design of Transonic Compressor Cascades with Stabilizing Elastic Surface Algorithm

The upgraded elastic surface algorithm (UESA) is a physical inverse design method that was recently developed for a compressor cascade with double-circular-arc blades. In this method, the blade walls are modeled as elastic Timoshenko beams that smoothly deform because of the difference between the t...

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Bibliographic Details
Main Authors: Mohammad Hossein Noorsalehi, Mahdi Nili-Ahmadabadi, Seyed Hossein Nasrazadani, Kyung-Chun Kim
Format: Article
Language:English
Published: MDPI AG 2021-05-01
Series:Applied Sciences
Subjects:
ESA
Online Access:https://www.mdpi.com/2076-3417/11/11/4845