Search
Search by keyword: "load reduction device"
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 |