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...
Main Authors: | , |
---|---|
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 |