Numerical Analysis of Aircraft Engine Fan Blade-Out-Reference-Cited by-同舟云学术

Numerical Analysis of Aircraft Engine Fan Blade-Out

Published:2006-07-09 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
language:
Short-container-title:

Author:

Shmotin Yuri,Gabov Dmitriy,Ryabov Alexander,Kukanov Sergey,Rechkin Vadim

Publisher

American Institute of Aeronautics and Astronautics

Reference4 articles.

1. 2Carney, K.S., Lawrence, C., Carney, D.V. "Aircraft Engine Blade-Out Dynamics," 7thInternational LS-DYNA Users Conference, 2001.

2. 5Ryabov,A.,Romanov,V.,Barkanov,B.,Skurikhin,S."NumericalSimulationsofDynamicDeformationofTransportSpent Fuel Package in Accidental Impact Loads," The 14th International Symposium on the Packaging and Transportation of Radioactive Materials, 2004.

Cited by 14 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Experimental and Numerical Study on the Perforation Behavior of an Aluminum 6061-T6 Cylindrical Shell;Materials;2023-11-06

2. Study of dynamic loads dependence on aircraft engine mount variant after fan blade-out event;Vibroengineering PROCEDIA;2019-09-26

3. Nonlinear Reduced Dynamic Model of Turbofan Engine for Investigation of Engine Structural Frame Vibrations After Fan Blade Out Event;Volume 7A: Structures and Dynamics;2019-06-17

4. Transient Analysis for a Twin Spool Rotor with Squeeze-Film Dampers Considering Blade Loss;Journal of Vibration Engineering & Technologies;2018-11-26

5. Investigation on the dynamic response of aero-engine structures due to fan blade out event through subscale testing;52nd AIAA/SAE/ASEE Joint Propulsion Conference;2016-07-22