Numerical and Experimental Verification of Spherically Layered Ice Model for Analysis on Hail Impacting Aviation Structures

Author:

Luo Gang12ORCID,Zhang Fengqi23,Cao Wanting23,Zhang Haiyang2,Liu Lulu23ORCID,Chen Wei23ORCID

Affiliation:

1. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

2. Key Laboratory of Impact Dynamics on Aero Engine, Liaoning Province 110000, China

3. Aero-engine Thermal Environment and Structure Key Laboratory of Ministry of Industry and Information Technology, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

Abstract

Aviation structures are required to be resistant to impact damage from hail. Therefore, aiming to gain a better understanding of such impacts, the formation mechanisms, spherically layered structures, and layer-density distributions of real hail were investigated. Based on analysis of the influence of different constitutive model parameters on the impact load on a metal target plate, a layered finite-element hail model was established, and this and several equivalent hail models were simulated and compared in terms of the dynamic responses during impact with a Ti6Al4V alloy plate target. The results showed that the characteristic values of the contact forces and impact displacements of spherically layered hail were lower than those for equivalent hailstones with the same mass or diameter. The spherically layered modeling of hail could provide a method for fine analysis of the phenomenology of hailstone impacts.

Funder

Fundamental Research Funds for the Central Universities

Publisher

Hindawi Limited

Subject

Aerospace Engineering

Reference35 articles.

1. Present status of investigation of foreign object damage to blade in aeroengine;G. U. A. N. Yupu;ACTA Aeronautica et Astronautica Sinica.,2007

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