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The Extension of the Range of Stable Operation of an Axial Compressor by Changing the Parameters of the Grids in the Terminal Zone of Blading
| Authors: Arkhipov D.V., Tumashev R.Z. | Published: 19.12.2017 |
| Published in issue: #12(693)/2017 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: axial compressor, high-pressure stage, gas-dynamic stability, diffusion, near-wall boundary layer |
