Experimental Study of Bowed-twisted Stators in an Axial Transonic Fan Stage
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Aerospace Engineering
Reference15 articles.
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3. Calvert W J, Emmerson P R, Moore J M. Design, test and analysis of a high-pressure-ratio transonic fan. ASME GT-2003-38302, 2003.
4. Effect of stator design on stator boundary layer flow in a highly loaded single-stage axial-flow low-speed compressor;Friedrichs;Journal of Turbomachinery,2001
5. Boese M, Fottner L. Effects of riblets on the loss behavior of a highly loaded compressor cascade. ASME GT-2002-30438, 2002.
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1. Application of the Symmetric Model to the Design Optimization of Fan Outlet Grills;Symmetry;2019-07-30
2. Studies on Downstream Stator with Rotor Re-Staggering and Forward Sweeping in a Subsonic Axial Compressor Stage;International Journal of Turbo & Jet-Engines;2014-01-01
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