• Rajal Shivraj Phulari
• S.K Swami

In the present paper, basic terminologies of laminated composite plates are discussed. In this project author discuss on to find the ‘u’ displacement in x direction for isotropic square and rectangle plate for simply supported and sinusoidal load and to find the warping effect in transverse direction for rectangular plate also the displacement in x, y, z direction for plate with loading condition. Laminated composite plate structures find numerous applications in aerospace, military and automotive industries. The role of transverse shear is very important in composites, as the material is weak in shear due to its low shear modulus compared to extensional rigidity. Hence, an accurate understanding of their structural behavior is required, such as deflections and stresses. From the present Literature Review the effect of bending, buckling, thermal & hydrothermal on composite plates discussed and different theories like Classical Plate Theory, First Order Shear Deformation Theory, and Higher order Shear Deformation Theory etc. for analysis of composite plate are mentioned.

U displacement in X direction, Higher Shear Deformation Theory.

"FORMATION OF LAMINATED COMPOSITE PLATE BY USING HIGHER SHEAR DEFORMATION THEORY.", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 6, page no.802-806, June 2019, Available :http://www.jetir.org/papers/JETIR1907L22.pdf

"FORMATION OF LAMINATED COMPOSITE PLATE BY USING HIGHER SHEAR DEFORMATION THEORY.", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 6, page no. pp802-806, June 2019, Available at : http://www.jetir.org/papers/JETIR1907L22.pdf