Modeling of flutter stability margins in an aerofoil cantilever wing with multiple engines mounts under inherent structural nonlinearities
This paper presents an aeroelastic analysis of aircraft wing having structural nonlinearities with two power plants subjected to time-dependent thrust loads in the event of failure of one of the engines. The equations of motion are derived based on continuous beam model of the wing system with two e...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Elsevier
2018-10-01
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| Series: | Engineering Science and Technology, an International Journal |
| Online Access: | http://www.sciencedirect.com/science/article/pii/S2215098617300320 |