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Methodology for Assessing Abrasive Particles Separation in the Axial Compressors Influencing Characteristics of the Aerial Vehicle Gas Turbine Engines: Dynamics Simulation in an Axial
Authors: Popov S.S., Cherkasov A.N., Klepikov D.S. | Published: 08.04.2025 |
Published in issue: #1(152)/2025 | |
DOI: | |
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
Keywords: erosion, wear, compressor, gas turbine engine, separator, CAD, ANSYS, CFD, CFX |