Dynamic Test of Bird Strike on a Flat Plate Made from LY-12 Aluminium

Jun  Liu; Zheng Li  Zhang

doi:10.4028/www.scientific.net/AMR.765-767.3158

Paper Titles

Property Research of Concrete Mixed with Flyash
p.3139

Microstructure and Properties of Alloys with Equal Atomic Principal Components
p.3143

Flutter Analysis of Composite Wing Using Differential Quadrature Method
p.3147

Research on Wellbore Stability in Formation with Anisotropic Strength
p.3151

Dynamic Test of Bird Strike on a Flat Plate Made from LY-12 Aluminium
p.3158

Properties of Freestanding Buckypapers with Monodispersion of Multi-Walled Carbon Nanotube Aqueous Solution
p.3162

Interfacial Properties for MEA and MEA-Water Mixtures
p.3166

Effect of Hydrothermal Reaction Conditions on the Sizes and Morphologies of ZnO Nanorods
p.3170

Microstructures and Mechanical Properties of AZ31+Sr+Y Magnesium Alloy Sheets Produced by Twin-Roll Casting and Sequential Hot Rolling
p.3176

HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 765-767Dynamic Test of Bird Strike on a Flat Plate Made...

Dynamic Test of Bird Strike on a Flat Plate Made from LY-12 Aluminium

Abstract:

Tests of bird strike have been carried out on plate made from LY-12 Aluminium. The test was down with the projectile impacting the target perpendicularly at velocity of 40m/s, 80m/s, 120m/s respectively. The displacement-time history curves and strain-time history curves of on LY-12 Aluminium plate were measured. The good agreement of the results between two specimens in one group indicated that the results tested in the presnet paper are reliable. The dynamic response of the plate and damage modes of the bird influenced by striking velocity were analyzed. The peak value of the displacement linear enlarged with the increasing of the striking velocity. The test results in the present paper provided valuable data for aircraft design impacted by bird, and also provided abundant test datas for the numerical simulation model applied in bird striking.

You might also be interested in these eBooks

View Preview

Info:

Periodical:

Advanced Materials Research (Volumes 765-767)

Pages:

3158-3161

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.765-767.3158

Citation:

Cite this paper

Online since:

September 2013

Authors:

Jun Liu, Zheng Li Zhang

Keywords:

Aluminium Plate, Bird Strike, Dynamic Test, LY-12

Export:

RIS, BibTeX

Price:

Permissions CCC:

Request Permissions

Permissions PLS:

Request Permissions

Сopyright:

Citation:

References

[1] S. T. Jenq, F. B. H. Siao, I.C. Lin, et al. Simulational of a rigid plate hit by a cylindrical hemi-spherical tip-ended soft impactor, Computational Materials Science [J], 39(2007): 518-526.

DOI: 10.1016/j.commatsci.2006.08.008

Google Scholar

[2] M.A. McCARTHY, J.R. XIAO, N. PETRINIC, et al. Modeling of Bird Strike on an Aircraft Wing Leading Edge Made from Fibre Metal Laminates-Part1: Material Modeling, Applied Composite Materials [J], 11(2004): 295-315.

DOI: 10.1023/b:acma.0000037133.64496.13

Google Scholar

[3] A. Airoldi, B. Cacchione. Modeling of impact forces and pressures in Lagrangian bird strike analysis, International Journal of Impact Engineering [J], 32(2006): 1651-1677.

DOI: 10.1016/j.ijimpeng.2005.04.011

Google Scholar

[4] Richard Budgey. The development of a substitute artificial bird by the international bird-strike research group for use in aircraft component testing. IBSC/WP-IE3, Amsterdam, 17-21 April (2000).

Google Scholar

[5] Alastair F. Johnson, Martin Holzapfel. Modelling soft body impact on composite structures. Composite Structures 61 (2003) 103-113.

DOI: 10.1016/s0263-8223(03)00033-3

Google Scholar

[6] Barber, J. P, Taylor, H.R. and Wilbeck, J.S., Bird impact force and pressures on rigid and compliant targets. Technical Report AFFDL-TR-77-60. Air Force Flight Dynamics Laboratory, May (1978).

Google Scholar