The Damage of Sandwich Composite Structure of Aircraft Radome under Debris-Strike

Xiao Qing Zhang; Xuan Liu

doi:10.4028/www.scientific.net/AMM.63-64.515

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 63-64The Damage of Sandwich Composite Structure of...

The Damage of Sandwich Composite Structure of Aircraft Radome under Debris-Strike

Abstract:

The low and medium speed impact damage of sandwich composite structure of aircraft radome shield under debris-strike during takeoff and landing along runway is examined by numerical simulations, using nonlinear dynamic finite element analysis software LS-DYNA. For different impact velocities, the dynamic responses of aircraft radome shield 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 design of aircraft radome.

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Periodical:

Applied Mechanics and Materials (Volumes 63-64)

Pages:

515-518

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.63-64.515

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Online since:

June 2011

Authors:

Xiao Qing Zhang, Xuan Liu

Keywords:

Aircraft Radome, Damage, Debris-Strike, Sandwich Composite Structure

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References

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