LARGE DEFLECTION BEHAVIOR OF QUASI-ISOTROPIC LAMINATES UNDER LOW-VELOCITY IMPACT TYPE POINT LOADING.

Ajit Kelkar; W. Elber; I. S. Raju

LARGE DEFLECTION BEHAVIOR OF QUASI-ISOTROPIC LAMINATES UNDER LOW-VELOCITY IMPACT TYPE POINT LOADING.

Ajit Kelkar
, W. Elber
, I. S. Raju

Mechanical Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

Abstract

Eight-ply quasi-isotropic circular composite plates of Thornel 300 graphite in Narmco 5208 epoxy resin (T300/5208) were analyzed to obtain the large deformation behavior under low-velocity impact type point loads. A simple plate-membrane coupling model was developed. The plate-membrane coupling model was used to obtain the large deformation shapes for the thin circular composite laminates. The plate-membrane coupling model was verified by conducting a series of tests on clamped circular quasi-isotropic laminates.

Original language	English
Title of host publication	Collection of Technical Papers - AIAA/ASME/ASCE/AHS 26th Structures, Structural Dynamics and Materials Conference.
Pages	432-441
Edition	pt 1
State	Published - 1985

Cite this

@inproceedings{0d41764240e043c3b8ccd1df2fe60305,

title = "LARGE DEFLECTION BEHAVIOR OF QUASI-ISOTROPIC LAMINATES UNDER LOW-VELOCITY IMPACT TYPE POINT LOADING.",

abstract = "Eight-ply quasi-isotropic circular composite plates of Thornel 300 graphite in Narmco 5208 epoxy resin (T300/5208) were analyzed to obtain the large deformation behavior under low-velocity impact type point loads. A simple plate-membrane coupling model was developed. The plate-membrane coupling model was used to obtain the large deformation shapes for the thin circular composite laminates. The plate-membrane coupling model was verified by conducting a series of tests on clamped circular quasi-isotropic laminates.",

author = "Ajit Kelkar and W. Elber and Raju, \{I. S.\}",

year = "1985",

language = "English",

pages = "432--441",

booktitle = "Collection of Technical Papers - AIAA/ASME/ASCE/AHS 26th Structures, Structural Dynamics and Materials Conference.",

edition = "pt 1",

}

LARGE DEFLECTION BEHAVIOR OF QUASI-ISOTROPIC LAMINATES UNDER LOW-VELOCITY IMPACT TYPE POINT LOADING. / Kelkar, Ajit; Elber, W.; Raju, I. S.
Collection of Technical Papers - AIAA/ASME/ASCE/AHS 26th Structures, Structural Dynamics and Materials Conference.. pt 1. ed. 1985. p. 432-441.

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

TY - GEN

T1 - LARGE DEFLECTION BEHAVIOR OF QUASI-ISOTROPIC LAMINATES UNDER LOW-VELOCITY IMPACT TYPE POINT LOADING.

AU - Kelkar, Ajit

AU - Elber, W.

AU - Raju, I. S.

PY - 1985

Y1 - 1985

N2 - Eight-ply quasi-isotropic circular composite plates of Thornel 300 graphite in Narmco 5208 epoxy resin (T300/5208) were analyzed to obtain the large deformation behavior under low-velocity impact type point loads. A simple plate-membrane coupling model was developed. The plate-membrane coupling model was used to obtain the large deformation shapes for the thin circular composite laminates. The plate-membrane coupling model was verified by conducting a series of tests on clamped circular quasi-isotropic laminates.

AB - Eight-ply quasi-isotropic circular composite plates of Thornel 300 graphite in Narmco 5208 epoxy resin (T300/5208) were analyzed to obtain the large deformation behavior under low-velocity impact type point loads. A simple plate-membrane coupling model was developed. The plate-membrane coupling model was used to obtain the large deformation shapes for the thin circular composite laminates. The plate-membrane coupling model was verified by conducting a series of tests on clamped circular quasi-isotropic laminates.

M3 - Conference contribution

SP - 432

EP - 441

BT - Collection of Technical Papers - AIAA/ASME/ASCE/AHS 26th Structures, Structural Dynamics and Materials Conference.

ER -

LARGE DEFLECTION BEHAVIOR OF QUASI-ISOTROPIC LAMINATES UNDER LOW-VELOCITY IMPACT TYPE POINT LOADING.

Abstract

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