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Computational study of characteristics of intake flow in model axial compressor with regard to different variants of “active disk” boundary condition
| Authors: Voronich I.V., Nguyen V.H. | Published: 20.05.2019 |
| Published in issue: #5(710)/2019 | |
| Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
| Keywords: turbojet engine, axial compressor air intake, active disk, variables profiles, computational technique |
