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Methodology for Assessing the Abrasive Particles Separation Effect in Axial Compressors on the Aviation Gas Turbine Engine Characteristics: Simulating Separation and Results
| Authors: Popov S.S., Cherkasov A.N., Klepikov D.S. | Published: 16.10.2025 |
| Published in issue: #3(154)/2025 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: compressor, gas turbine engine, separator, setup, CAD, ANSYS, CFD, Fluent | |