Possibility of using a bi-directional impulse turbine in a thermo-acoustic engine
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Thermo-mechanical modeling of a high pressure turbine blade of an airplane gas turbine engine
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ژورنال
عنوان ژورنال: VESTNIK of the Samara State Aerospace University
سال: 2015
ISSN: 1998-6629
DOI: 10.18287/1998-6629-2015-14-1-132-138