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Aeronautical Manufacturing Technology  2019, Issue (10): 78-82    DOI: 10.16080/j.issn1671-833x.2019.10.078
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Transition Section of Turbine Blade Modeling Method Fitting Bowed-Twist Wall
CHEN Yang1, ZHAO Xiaoci1, XI Ping1, XU Jingliang2
1. School of Mechanical Engineering and Automation, Beihang University, Beijing 100191, China;
2. AECC Shenyang Engine Research Institute, Shenyang 110000, China
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