ASSESSMENT RESULTS OF THE DYNAMIC STABILITY FOR SUBSONIC FLUTTER OF THE BLADE ASSEMBLIES OF THE COMPRESSORS OF SOME AIRCRAFT GAS-TURBINE ENGINES
The paper outlines the results of the investigation on the verification of the express method of prediction of dynamic stability for subsonic flutter using the blade assemblies of individual stages of the compressor of some types of aircraft gas-turbine engines at different modes of their operation....
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
National Aerospace University «Kharkiv Aviation Institute»
2019-08-01
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| Series: | Авіаційно-космічна техніка та технологія |
| Subjects: | |
| Online Access: | http://nti.khai.edu/ojs/index.php/aktt/article/view/871 |