Investigation on the dynamic response of aero-engine structures due to fan blade out event through subscale testing
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4861
Reference17 articles.
1. Aeroengine turbine blade containment tests using high-speed rotor spin testing facility
2. Perforation of aero-engine fan casing by a single rotating blade
3. Multi-blade effects on aero-engine blade containment
4. Blade loss transient dynamic analysis of turbomachinery
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1. Containment of blade shedding in gas turbine engines: part II—experimental and numerical investigations;International Journal of Mechanics and Materials in Design;2020-08-25
2. Containment of blade shedding in gas turbine engines: part I—design and development of a scaled down test rig;International Journal of Mechanics and Materials in Design;2020-08-24
3. The numerical modeling of rotor–stator rubbing in rotating machinery: a comprehensive review;Nonlinear Dynamics;2020-07
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