THE STUDY OF PART FRACTURE TOUGHNESS UNDER THE THERMAL PULSE LOADING

The cracking problem of aviation unit part under the influence of the thermal pulse loading were considered. The problem of thermal plasticity during thermal pulse processing were solved in CAE system Ansys; internal stresses were calculated and stress concentration zones in the part were defined. A...

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Bibliographic Details
Main Authors: Ольга Владимировна Шипуль, Игорь Борисович Кузнецов, Григорий Сергеевич Тевзадзе, Роман Александрович Ходак
Format: Article
Language:English
Published: National Aerospace University «Kharkiv Aviation Institute» 2017-01-01
Series:Авіаційно-космічна техніка та технологія
Subjects:
Online Access:http://nti.khai.edu/ojs/index.php/aktt/article/view/480