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On the choice of parameters of device to reduce load on components of turbojet engine pressure vessels after fan blade breakage
| Authors: Ivanov I.I. | Published: 27.05.2015 |
| Published in issue: #10(631)/2012 | |
| Category: Calculation and Design of Machinery | |
| Keywords: gas-turbine engine, load reduction device, rotor, fan blade, breakage |
