Numerical Analysis of the Influences of Geometrical Deviation on Delamination in Composite Laminates around the Countersunk Hole

Joint Authors

Liu, Xueshu
Yang, Yuxing
Gao, Hang
Huang, Li
Zhang, Ping

Source

International Journal of Aerospace Engineering

Issue

Vol. 2018, Issue 2018 (31 Dec. 2018), pp.1-11, 11 p.

Publisher

Hindawi Publishing Corporation

Publication Date

2018-01-14

Country of Publication

Egypt

No. of Pages

11

Abstract EN

During countersunk hole machining, defects like geometrical deviation of the chamfer angle and delamination are easily introduced into the structure.

To investigate the influences of geometrical deviation on delamination propagation around the countersunk hole during assembly, a progressive damage model (PDM) combining cohesive element was proposed and validated.

Numerical analyses were then carried out to study delamination propagation behavior under the influences of geometrical parameters including delamination factor, chamfer angle, and location of delamination.

The results show that when delamination appears at the transition area of the countersunk hole, the load causing the delamination evolution is much smaller than other cases.

American Psychological Association (APA)

Liu, Xueshu& Yang, Yuxing& Huang, Li& Zhang, Ping& Gao, Hang. 2018. Numerical Analysis of the Influences of Geometrical Deviation on Delamination in Composite Laminates around the Countersunk Hole. International Journal of Aerospace Engineering،Vol. 2018, no. 2018, pp.1-11.
https://search.emarefa.net/detail/BIM-1167303

Modern Language Association (MLA)

Liu, Xueshu…[et al.]. Numerical Analysis of the Influences of Geometrical Deviation on Delamination in Composite Laminates around the Countersunk Hole. International Journal of Aerospace Engineering No. 2018 (2018), pp.1-11.
https://search.emarefa.net/detail/BIM-1167303

American Medical Association (AMA)

Liu, Xueshu& Yang, Yuxing& Huang, Li& Zhang, Ping& Gao, Hang. Numerical Analysis of the Influences of Geometrical Deviation on Delamination in Composite Laminates around the Countersunk Hole. International Journal of Aerospace Engineering. 2018. Vol. 2018, no. 2018, pp.1-11.
https://search.emarefa.net/detail/BIM-1167303

Data Type

Journal Articles

Language

English

Notes

Includes bibliographical references

Record ID

BIM-1167303