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Effect of Pitch Angle on the Strength of a TC4/Helicoidal Composite Double-Bolt Scarf Joint: A Numerical Study
by
Zhang, Guofan
, Wan, Chunhua
, Du, Xin
, Yu, Zhefeng
, Lian, Xin
in
Aluminum
/ Bolted joints
/ Composite materials
/ Cracks
/ Damage assessment
/ Failure analysis
/ Failure load
/ Failure mechanisms
/ Failure modes
/ Finite element method
/ Laminates
/ Load
/ Mathematical models
/ Pitch (inclination)
/ Scarf joints
/ Simulation
/ Stress analysis
/ Tensile tests
/ Ultimate loads
2025
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Effect of Pitch Angle on the Strength of a TC4/Helicoidal Composite Double-Bolt Scarf Joint: A Numerical Study
by
Zhang, Guofan
, Wan, Chunhua
, Du, Xin
, Yu, Zhefeng
, Lian, Xin
in
Aluminum
/ Bolted joints
/ Composite materials
/ Cracks
/ Damage assessment
/ Failure analysis
/ Failure load
/ Failure mechanisms
/ Failure modes
/ Finite element method
/ Laminates
/ Load
/ Mathematical models
/ Pitch (inclination)
/ Scarf joints
/ Simulation
/ Stress analysis
/ Tensile tests
/ Ultimate loads
2025
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Effect of Pitch Angle on the Strength of a TC4/Helicoidal Composite Double-Bolt Scarf Joint: A Numerical Study
by
Zhang, Guofan
, Wan, Chunhua
, Du, Xin
, Yu, Zhefeng
, Lian, Xin
in
Aluminum
/ Bolted joints
/ Composite materials
/ Cracks
/ Damage assessment
/ Failure analysis
/ Failure load
/ Failure mechanisms
/ Failure modes
/ Finite element method
/ Laminates
/ Load
/ Mathematical models
/ Pitch (inclination)
/ Scarf joints
/ Simulation
/ Stress analysis
/ Tensile tests
/ Ultimate loads
2025
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Effect of Pitch Angle on the Strength of a TC4/Helicoidal Composite Double-Bolt Scarf Joint: A Numerical Study
Journal Article
Effect of Pitch Angle on the Strength of a TC4/Helicoidal Composite Double-Bolt Scarf Joint: A Numerical Study
2025
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Overview
A progressive damage model was developed to study the damage and failure behavior of CFRP/Ti double-bolt scarf joints under quasi-static loading. The three-dimensional Hashin failure criterion was integrated into a finite element model via the ABAQUS user-defined material subroutine. Quasi-static tensile tests were conducted to investigate failure mechanisms and validate the model. The predicted failure modes match the experimental results with an error of 11.8% in the prediction of ultimate load. The effect of helicoidal layup on the composite joint was studied for the application of a helicoidal composite. The results show that the helicoidal layup configuration with a 45/−45 layup on the surface had the highest failure load, and the helicoidal layup introduced more tensile damage in the matrix. This study offers practical failure prediction methods and comprehensive failure mode analysis for composite bolted scarf joints.
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