DIFFERENCES BETWEEN GRAPHENE-BASED COMPOSITE MATERIALS AND CONVENTIONAL MATERIALS IN AIRCRAFT STRUCTURAL ELEMENTS

Authors

  • N. A. Abdujabarov Doctor of Philosophy (PhD), Head of the “Aviation Engineering” Department, Faculty of Aviation Transport Engineering, Tashkent State Transport University Author
  • B. A. Nomozov Independent Researcher of the “Aviation Engineering” Department, Faculty of Aviation Transport Engineering, Tashkent State Transport University Author

Keywords:

Graphene, nanocomposite, aviation materials, strength, density, Young’s modulus, aerospace technology, lightweight structures

Abstract

This article analyzes the differences between graphene-based composite materials used in aircraft structural elements and conventional aviation materials (aluminum, titanium, steel, and carbon fiber composites) using a comprehensive scientific approach. The physical, mechanical, thermal, and operational properties of these materials are compared using numerical data. In addition, the impact of graphene-based composites on the aviation industry, their economic efficiency, and technological limitations are discussed.

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Published

2026-05-23

Issue

Vol. 2 No. 5 (2026)

Section

Articles

License

Creative Commons License

This work is licensed under a Creative Commons Attribution 4.0 International License.