ADVANCED COMPOSITE WING DESIGN AND FINITE ELEMENT STRUCTURAL ANALYSIS

Authors

  • Dr.S.Reehana Author
  • Dr. D. Ramana Reddy Author
  • V.Lokesh Vardhan Author

Keywords:

Advanced Composite Materials, Wing Design, Finite Element Analysis (FEA), Structural Optimization, Stress Analysis, Deformation, Aerospace Structures, Carbon Fiber Reinforced Polymer (CFRP), Load Distribution, Aircraft Performance

Abstract

Advanced composite wing design and finite element structural analysis are implemented in this investigation to enhance the efficiency, durability, and utility of existing aircraft structures. Because of their higher strength-to-weight ratios, fatigue resistance, and corrosion resistance, composite materials—like carbon fiber reinforced polymers—often replace conventional metal structures. This study uses complicated wing models and Finite Element Analysis (FEA) to assess stress distribution, wing deformation, and the maximum weight that the wings can support under various wind and structural loading situations. In order to minimize a structure's weight, optimization techniques are used to improve its architecture and material usage. Dependability and security are guaranteed. The findings imply that modern composite wing designs significantly enhance an aircraft's overall performance and structural efficiency. This demonstrates their potential significance in the aviation engineering area.

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Author Biographies

  • Dr.S.Reehana

    Professor in Mechanical, VISWAM ENGINEERING COLLEGE, MADANAPALLI, AP.

  • Dr. D. Ramana Reddy

    Professor in Mechanical & Principal, VISWAM ENGINEERING COLLEGE, MADANAPALLI, AP.

  • V.Lokesh Vardhan

    PG Student in Mechanical Department, VISWAM ENGINEERING COLLEGE, MADANAPALLI, AP.

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Published

2026-05-19

Issue

Vol. 2 No. 2 (2026): Volume 2, Issue 2 , April-June, 2026

Section

Articles

License

Copyright (c) 2026 Journal of Engineering Excellence

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