Maximum Thickness Location Selection of High Subsonic Axial Compressor Airfoils and Its Effect on Aerodynamic Performance

Overview of attention for article published in Frontiers in Energy Research, November 2021

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New Research: Maximum Thickness Location Selection of High Subsonic Axial Compressor Airfoils and Its Effect on Aerodynamic Performance: Solidity and camber angle are key parameters with a primary effect on airfoil diffusion. Maximum… https://t.co/Zra05ll0

22 Nov 2021

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