2019
DOI: 10.1063/1.5085609
|View full text |Cite
|
Sign up to set email alerts
|

Determination of residual stresses in GFRP composite using incremental slitting method by the aid of strain gauge

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1
1

Citation Types

1
4
0

Year Published

2021
2021
2022
2022

Publication Types

Select...
5

Relationship

0
5

Authors

Journals

citations
Cited by 5 publications
(5 citation statements)
references
References 20 publications
1
4
0
Order By: Relevance
“…Under these conditions, the stresses along the fibers reached 40-60 MPa. Similar results substantiating the formation of cracks, shrinkage, and interlayer fracture were obtained in [26,[33][34][35][36][37].…”
Section: Causes For Internal Stresses In Pcmssupporting
confidence: 86%
“…Under these conditions, the stresses along the fibers reached 40-60 MPa. Similar results substantiating the formation of cracks, shrinkage, and interlayer fracture were obtained in [26,[33][34][35][36][37].…”
Section: Causes For Internal Stresses In Pcmssupporting
confidence: 86%
“…Various methods for creating the slit have been used from the basic approach of using a thin saw blade [14,[48][49][50][51][52] to using focused ion beams [42,46,53,54] and an electron discharge machine (EDM). [45,55] One obvious problem of using a saw, a mill or any other abrasive method is that it will invariably introduce additional stresses into the specimen being tested.…”
Section: The Slitting Methodsmentioning
confidence: 99%
“…Destructive methods of residual stress measurements are based on the principle of estimating stresses from deformations/strains, which are released when the stressed specimen is locally machined. The slitting method [ 15 , 16 , 17 , 18 , 19 , 20 , 21 , 22 , 23 , 24 , 25 ], also known as the crack compliance method, is one of the most commonly used destructive methods. It involves machining a narrow slit through a stressed sample and the released strains are measured using a strain gage bonded across the adjacent material.…”
Section: Mechanical Testsmentioning
confidence: 99%
“…The recorded strains and the residual stresses for each incremental cut can be expressed in matrix form as: where [ C ] is the compliance coefficient matrix, is the vector of residual stress and —vector of recorded strain compliance coefficients were determined by simulating the experimental slitting process of the composite specimen using FE analysis. The simulation was carried out using ANSYS software with the experimentally determined elastic constants of GE and CE laminates* using the procedure detailed in the earlier reported works [ 13 , 18 , 20 , 21 , 22 , 23 , 24 , 25 ]. The specific element of compliance matrix C ij corresponds to strains measured across the strain gauge when the applied residual stresses are equal to the unit load.…”
Section: Mechanical Testsmentioning
confidence: 99%