Numerical study of flows in axial compressors of aircraft gas-turbine engines
Design and adjustment of compressors at modern gas-turbine engines are based on the wide use of numerical analysis methods of a various level of complexity. Such approaches make it possible to analyze the alignment of joint operation of stages and to perform the required correction of geometrical pa...
| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
PC Technology Center
2018-07-01
|
| Series: | Eastern-European Journal of Enterprise Technologies |
| Subjects: | |
| Online Access: | http://journals.uran.ua/eejet/article/view/139445 |