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클램핑 포스가 존재하는 복합재료 체결부의 파손강도 예측

Failure load prediction of mechanically fastened composite joint with the clamping force

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참고문헌

키워드

주제분류재료공학

초록

Abstract

The design of composite joint is a very important research area because they are often the weakest areas in composite structures. In this paper, the failure load of the mechanically fastened composite joint with the clamping force was predicted by the failure area index method. By the suggested failure area index method, the strength of the mechanically fastened composite joint could be predicted within 22.5% when the clamping force was applied to the composite joint.

참고문헌 (13)

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  2. "Stress Fracture Criteria for Laminated Composites Containing Stress Concentrations", pp.~8
  3. "Uniaxial Failure of Composite Laminated Containing Stress Concentrations"
  4. "Strength of Mechanically Fastened Composite Joints", pp.~16
  5. "Failure of Composite Laminates Containing Pin Loaded Holes-Method of Solution", pp.~18
  6. ""The response of Composite Joints with Bolt-Clamping Loads, Part Ⅰ: Model Development"", 36, pp.47~67 (2002)
  7. "The response of Composite Joints with Bolt-Clamping Loads, Part Ⅱ: Model Verification", 36, pp.69~92 (2002)
  8. "기계적으로 체결된 복합재료 조인트의 강도에 관한 연구", 15(4), pp.9~16 (2002)
  9. "파괴면적지수법을 이용한 복합재료 기계적 체결부의 강도평가에 관한 연구", 16(5), pp.1~6 (2003)
  10. "Failure Load Prediction of Mechanically Fastened Composite Joint", 37(24), pp.2163~2177
  11. "Bearing Failure of Bolted Composite Joints. Part I : Experimental Characterization", 30(12) (1996)
  12. "Strength Envelope of Bolted Composite Joints under Bypass Loads", 30(13) (1996)
  13. "A prediction method for the compressive strength of impact damaged composite laminates", 30, pp.357~367 (1995)

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