Simulation for the Bird-Strike Damage of Drone Radome Composite Structure

Yan Bin He; Xiao Hu Yao; Xuan Liu; Ling Feng He

doi:10.4028/www.scientific.net/AMM.151.305

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vol. 151Simulation for the Bird-Strike Damage of Drone...

Simulation for the Bird-Strike Damage of Drone Radome Composite Structure

Abstract:

The low and medium speed bird-strike impact damage of sandwich composite structure of drone radome during takeoff and landing is examined by numerical simulations, using nonlinear dynamic finite element analysis software LS-DYNA. For different impact velocities, the aircraft radome’s dynamic responses are obtained and the damage in composite panel is clearly demonstrated. The relations of impact energy, maximum impact force and the damage state are analyzed. The simulation results can provide some references for the aircraft radome design.

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Periodical:

Applied Mechanics and Materials (Volume 151)

Pages:

305-309

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.151.305

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Online since:

January 2012

Authors:

Yan Bin He, Xiao Hu Yao, Xuan Liu, Ling Feng He

Keywords:

Aircraft Radome, Bird-Strike, Finite Element, Low Energy Damage, Sandwich Composite Structure

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