Ajaykumar Thakur

Prof. Ajaykumar Thakur

Mechanical Engineering, Sanjivani College of Engineering, Kopargaon, Ahmednagar, India
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Research Focus & Metrics

Academic Career Length

14Years (2013-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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1 January 2018 in Materials Today: Proceedings
Verified
Journal Article
Closed access
Kiran WakchaureKiran Wakchaure
Kiran Wakchaure
ATAjaykumar Thakur
Ajaykumar Thakur
Vijay Shivaji GadakhVijay Shivaji Gadakh
Vijay Shivaji Gadakh
AKA. Kumar
A. Kumar

3 September 2013 in Arabian Journal for Science and Engineering
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Journal Article
Closed access
PDF file
ATAjaykumar Thakur
Ajaykumar Thakur
VNV. M. Nandedkar
V. M. Nandedkar

1 January 2021 in Materials Today: Proceedings
Verified
Journal Article
Closed access
STS.R. Thorat
S.R. Thorat
ATAjaykumar Thakur
Ajaykumar Thakur

1 January 2018 in Materials Today: Proceedings
Verified
Journal Article
Closed access
STS.R. Thorat
S.R. Thorat
ATAjaykumar Thakur
Ajaykumar Thakur


19 September 2021 in International Journal of Automotive and Mechanical Engineering
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Journal Article
Open access
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DBDhiraj Bhaskar
Dhiraj Bhaskar
ATAjaykumar Thakur
Ajaykumar Thakur
ISImran I. Sayyad
Imran I. Sayyad
SBSantosh V. Bhaskar
Santosh V. Bhaskar
In this work, using new inverse trigonometric kinematic displacement function, the bending solution of simply supported isotropic and transversely isotopic thin, moderately thin and thick square plates with aspect ratio variations is given. The paper introduces a new inverse trigonometric shear deformation theory (nITSDT) for the bi-directional bending study, which is variationally compatible. The transverse shear stress can be obtained directly from the constitutive relationships on the top and bottom surfaces of the plate that satisfy the shear stress free surface conditions, so the theory does not need a factor for shear correction. The dynamic version of the virtual work principle is used to obtain the governing equations and boundary conditions of the theory. The Finite Element (FE) solution has been developed using MATLAB code based on the present theory for simply supported laminated composite plates. In order to illustrate the efficiency of the proposed theory, the results of displacements and stresses are compared with those of other refined theories and exact solution. The findings obtained from the use of the theory are found to agree well with the precise results of elasticity.