STATISTICAL ANALYSIS OF DAMAGEABILITY OF THE BYPASS ENGINES COMPRESSOR BLADES

Aircraft gas turbine engines during the operation are exposed to damage of flowing parts. The elements of the engine design, appreciably determining operational characteristics are rotor blades. Character of typical damages for various types of engines depends on appointment and a geographical place...

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Bibliographic Details
Main Authors: B. A. Chichkov, M. A. Zaiats
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2018-03-01
Series:Naučnyj Vestnik MGTU GA
Subjects:
Online Access:https://avia.mstuca.ru/jour/article/view/1197