International Journal of Vehicle Structures and Systems

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Analysis of Axial Crack in Aircraft Fuselage Circumferential Joint Using Finite Element Simulation


Affiliations
1 Dept. of Mech. Engg., Dayananda Sagar College of Engineering, Bengaluru, India
2 Dept. of Mech. Engg., B.N.M. Institute of Technology, Bengaluru, India
 

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Ring frames, stringers and skin panels are the main parts of aircraft fuselage structure. Circumferential joint is formed by joining skin panels in circumferential direction using doubler plates and adhesive bonding. In this paper finite element (FE) modeling of circumferential butt joint of fuselage structure using commercial FEA software (ANSYS) is presented. The FE model is validated using a benchmark and then fracture mechanics results are graphically presented and discussed.

Keywords

Circumferential Joint, Crack, Finite Element Modelling, Aircraft Fuselage Structure, Structural Integrity.
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Abstract Views: 486

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  • Analysis of Axial Crack in Aircraft Fuselage Circumferential Joint Using Finite Element Simulation

Abstract Views: 486  |  PDF Views: 211

Authors

H. Ramesha
Dept. of Mech. Engg., Dayananda Sagar College of Engineering, Bengaluru, India
N. C. Mahendra Babu
Dept. of Mech. Engg., B.N.M. Institute of Technology, Bengaluru, India
H. V. Lakshminarayana
Dept. of Mech. Engg., Dayananda Sagar College of Engineering, Bengaluru, India

Abstract


Ring frames, stringers and skin panels are the main parts of aircraft fuselage structure. Circumferential joint is formed by joining skin panels in circumferential direction using doubler plates and adhesive bonding. In this paper finite element (FE) modeling of circumferential butt joint of fuselage structure using commercial FEA software (ANSYS) is presented. The FE model is validated using a benchmark and then fracture mechanics results are graphically presented and discussed.

Keywords


Circumferential Joint, Crack, Finite Element Modelling, Aircraft Fuselage Structure, Structural Integrity.



DOI: https://doi.org/10.4273/ijvss.6.4.03