Progressive matrix cracking of crossply composite laminates under biaxial loading

C. L. Tsai; I. M. Daniel; J. W. Lee

Progressive matrix cracking of crossply composite laminates under biaxial loading

C. L. Tsai^*, I. M. Daniel, J. W. Lee

^*Corresponding author for this work

Civil and Environmental Engineering

Research output: Contribution to journal › Conference article › peer-review

23 Scopus citations

Abstract

An interlaminar-shear-stress analysis for progressive damage in composite laminates was developed. A general governing equation set was derived for [φ_m/θ_n]_s laminates that involves only in-plane displacements in both layers based on equilibrium, continuity and boundary conditions. The case of the crossply [0_m/90_n]_s laminate with matrix cracks in both layers under biaxial loading was solved. Residual stresses and non-linear behavior were taken into consideration. Theoretical predictions agree fairly well with experimental data in many ways. Stress distributions for various crack densities were obtained.

Original language	English (US)
Pages (from-to)	9-18
Number of pages	10
Journal	American Society of Mechanical Engineers, Applied Mechanics Division, AMD
Volume	111
State	Published - 1990
Event	Winter Annual Meeting of the American Society of Mechanical Engineers - Dallas, TX, USA Duration: Nov 25 1990 → Nov 30 1990

ASJC Scopus subject areas

Mechanical Engineering

Cite this

@article{81e676d36d6a4a278e720a9a9a9c91c2,

title = "Progressive matrix cracking of crossply composite laminates under biaxial loading",

abstract = "An interlaminar-shear-stress analysis for progressive damage in composite laminates was developed. A general governing equation set was derived for [φm/θn]s laminates that involves only in-plane displacements in both layers based on equilibrium, continuity and boundary conditions. The case of the crossply [0m/90n]s laminate with matrix cracks in both layers under biaxial loading was solved. Residual stresses and non-linear behavior were taken into consideration. Theoretical predictions agree fairly well with experimental data in many ways. Stress distributions for various crack densities were obtained.",

author = "Tsai, {C. L.} and Daniel, {I. M.} and Lee, {J. W.}",

year = "1990",

language = "English (US)",

volume = "111",

pages = "9--18",

journal = "American Society of Mechanical Engineers, Applied Mechanics Division, AMD",

issn = "0160-8835",

note = "Winter Annual Meeting of the American Society of Mechanical Engineers ; Conference date: 25-11-1990 Through 30-11-1990",

}

TY - JOUR

T1 - Progressive matrix cracking of crossply composite laminates under biaxial loading

AU - Tsai, C. L.

AU - Daniel, I. M.

AU - Lee, J. W.

PY - 1990

Y1 - 1990

N2 - An interlaminar-shear-stress analysis for progressive damage in composite laminates was developed. A general governing equation set was derived for [φm/θn]s laminates that involves only in-plane displacements in both layers based on equilibrium, continuity and boundary conditions. The case of the crossply [0m/90n]s laminate with matrix cracks in both layers under biaxial loading was solved. Residual stresses and non-linear behavior were taken into consideration. Theoretical predictions agree fairly well with experimental data in many ways. Stress distributions for various crack densities were obtained.

AB - An interlaminar-shear-stress analysis for progressive damage in composite laminates was developed. A general governing equation set was derived for [φm/θn]s laminates that involves only in-plane displacements in both layers based on equilibrium, continuity and boundary conditions. The case of the crossply [0m/90n]s laminate with matrix cracks in both layers under biaxial loading was solved. Residual stresses and non-linear behavior were taken into consideration. Theoretical predictions agree fairly well with experimental data in many ways. Stress distributions for various crack densities were obtained.

UR - http://www.scopus.com/inward/record.url?scp=0025558796&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=0025558796&partnerID=8YFLogxK

M3 - Conference article

AN - SCOPUS:0025558796

VL - 111

SP - 9

EP - 18

JO - American Society of Mechanical Engineers, Applied Mechanics Division, AMD

JF - American Society of Mechanical Engineers, Applied Mechanics Division, AMD

SN - 0160-8835

T2 - Winter Annual Meeting of the American Society of Mechanical Engineers

Y2 - 25 November 1990 through 30 November 1990

ER -

Progressive matrix cracking of crossply composite laminates under biaxial loading

Abstract

ASJC Scopus subject areas

Other files and links

Fingerprint

Cite this