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International Journal of Aerospace Engineering
Volume 2015, Article ID 312430, 6 pages
Research Article

Solution of Turbine Blade Cascade Flow Using an Improved Panel Method

Department of Aerospace Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

Received 27 September 2015; Revised 19 November 2015; Accepted 22 November 2015

Academic Editor: Linda L. Vahala

Copyright © 2015 Zong-qi Lei and Guo-zhu Liang. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

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