Tip-leakage flow loss reduction in a two-stage turbine using axisymmetric-casing contouring
نویسندگان
چکیده
منابع مشابه
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ژورنال
عنوان ژورنال: Chinese Journal of Aeronautics
سال: 2014
ISSN: 1000-9361
DOI: 10.1016/j.cja.2014.08.009