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Proceedings of the International Conference on Modern Research in Aerospace Engineering pp 203–210Cite as

Behavior of Rectangular Laminated Composite Plate with Central Hole Under Transverse Loading

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Part of the book series: Lecture Notes in Mechanical Engineering ((LNME))

Abstract

The present paper reports behavior of rectangular laminated composite plates with central circular hole and without hole under transverse loading. The plates used in the present study are laminated composite plates of epoxy resin reinforced with E-glass fiber. The laminates of symmetric and antisymmetric have been used in the study. Parameter used for the analysis is hole diameter to width of the plate ratio (D/H). The ratio used for the study varies from 0.1 to 0.5 with an increment of 0.1. The thickness of the composite plate is kept equal in all loading cases. Stresses and deflections in the plate are considered using boundary conditions of clamped edges. The results were discussed critically on the basis of variation of D/H versus stresses and D/H versus deflection.

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Abbreviations

E1, E2, E3 :

moduli of elasticity of lamina x, y, and z directions

G12, G23, G13 :

shear moduli of a lamina in xy, yz, and xz directions

μ12, μ23, μ13 :

Poison’s ratio in xy, yz, and xz directions

1, 2, 3:

x, y, and z directions

D/H:

hole diameter to width of the plate

References

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Author information

Authors and Affiliations

  1. Department of Civil Engineering, Amity University, Noida, 201313, Uttar Pradesh, India

    Sumit Rathi, Yogesh Kaushik & Sabita Madhvi Singh

Authors
  1. Sumit Rathi
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  2. Yogesh Kaushik
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  3. Sabita Madhvi Singh
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Corresponding author

Correspondence to Yogesh Kaushik .

Editor information

Editors and Affiliations

  1. Amity Institute of Aerospace Engineering, Amity University, Noida, Uttar Pradesh, India

    Sanjay Singh

  2. DTC Secretariat, Ghaziabad, Uttar Pradesh, India

    Pushkar Raj

  3. Department of Aerospace Engineering and Engineering Mechanics, College of Engineering and Applied Sciences, University of Cincinnati, Cincinnati, Ohio, USA

    Samir Tambe

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© 2018 Springer Nature Singapore Pte Ltd.

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Cite this paper

Rathi, S., Kaushik, Y., Singh, S.M. (2018). Behavior of Rectangular Laminated Composite Plate with Central Hole Under Transverse Loading. In: Singh, S., Raj, P., Tambe, S. (eds) Proceedings of the International Conference on Modern Research in Aerospace Engineering. Lecture Notes in Mechanical Engineering. Springer, Singapore. https://doi.org/10.1007/978-981-10-5849-3_21

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  • DOI: https://doi.org/10.1007/978-981-10-5849-3_21

  • Published:

  • Publisher Name: Springer, Singapore

  • Print ISBN: 978-981-10-5848-6

  • Online ISBN: 978-981-10-5849-3

  • eBook Packages: EngineeringEngineering (R0)

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