DEVELOPMENT OF METHODOLOGY FOR PREDICTING FATIGUE LIFE OF FIBER REINFORCED METAL LAMINATES

doi:10.6052/1000-0992-1999-3-J1998-085

Volume 29 Issue 3

Aug. 1999

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Article Navigation > Advances in Mechanics > 1999 > 29(3): 304-316

DEVELOPMENT OF METHODOLOGY FOR PREDICTING FATIGUE LIFE OF FIBER REINFORCED METAL LAMINATES[J]. Advances in Mechanics, 1999, 29(3): 304-316. doi: 10.6052/1000-0992-1999-3-J1998-085

Citation:

DEVELOPMENT OF METHODOLOGY FOR PREDICTING FATIGUE LIFE OF FIBER REINFORCED METAL LAMINATES[J]. Advances in Mechanics, 1999, 29(3): 304-316. doi: 10.6052/1000-0992-1999-3-J1998-085

DEVELOPMENT OF METHODOLOGY FOR PREDICTING FATIGUE LIFE OF FIBER REINFORCED METAL LAMINATES[J]. Advances in Mechanics, 1999, 29(3): 304-316. doi: 10.6052/1000-0992-1999-3-J1998-085

Citation:

DEVELOPMENT OF METHODOLOGY FOR PREDICTING FATIGUE LIFE OF FIBER REINFORCED METAL LAMINATES[J]. Advances in Mechanics, 1999, 29(3): 304-316. doi: 10.6052/1000-0992-1999-3-J1998-085

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DEVELOPMENT OF METHODOLOGY FOR PREDICTING FATIGUE LIFE OF FIBER REINFORCED METAL LAMINATES

doi: 10.6052/1000-0992-1999-3-J1998-085

北京航空材料研究院

Publish Date: 1999-08-25

Abstract

Abstract

The paper presents a review of the characteristics of a new group of aircraft materials,the fiber reinforced metal laminates (FRMLs), the mechanism of fatigue damage, and the industrial application. Several important issues, including the bridging stress, the delamination growth and the prediction of the fatigue crack growth rates and the fatigue life, were addressed and summarized. Some suggestions on the prediction of fatigue life were proposed.
- fiber reinforced metal laminates,
- damage,
- bridging traction,
- crack growth,
- delamination growth,
- fatigue life prediction