Use of computational fluid dynamics to implement an aerodynamic inverse design method based on exact Riemann solution and moving wall boundary
Author:
Affiliation:
1. College of Power and Energy Engineering, Harbin Engineering University, Harbin, People’s Republic of China
Publisher
Informa UK Limited
Subject
Modeling and Simulation,General Computer Science
Link
https://www.tandfonline.com/doi/pdf/10.1080/19942060.2020.1711812
Reference25 articles.
1. Arbabi, A. & Ghaly, W. (2013). Inverse design of turbine and compressor stages using a commercial CFD program. In ASME. Turbo Expo: Power for land, sea, and air, Volume 6B: Turbomachinery. San Antonio, USA.
2. Arbabi, A., Ghaly, W. & Medd, A. (2017). Aerodynamic inverse blade design of axial compressors in three-dimensional flow using a commercial CFD program. In ASME. Turbo Expo: Power for land, sea, and air, Volume 2B: Turbomachinery. Charlotte, USA.
3. Unsteady Euler airfoil solutions using unstructured dynamic meshes
4. Bell, R. M. & Fottner, L. (1995). Investigations of shock/ boundary-layer interaction in a highly loaded compressor cascade. In ASME. Turbo Expo: Power for land, sea, and air, Volume 1: Turbomachinery. Houston, USA.
5. A Three-Dimensional Inverse Method for Turbomachinery: Part I—Theory
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