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Sumit Nayair

Department of Aerospace Engineering, India


  • Mini Review   
    Computational Analysis of Aerodynamic Performance and Structural Integrity of a Novel Aircraft Wing Design
    Author(s): Sumit Nayair*

    This research article presents a comprehensive computational analysis of the aerodynamic performance and structural integrity of a novel aircraft wing design. The study employs advanced simulation techniques to assess the feasibility and potential advantages of the proposed wing configuration. Computational fluid dynamics (CFD) simulations are utilized to evaluate the aerodynamic efficiency, lift-to-drag ratio, and flow characteristics of the new wing design. Additionally, finite element analysis (FEA) is employed to investigate the structural integrity and load-bearing capabilities of the wing under various flight conditions. The results highlight the potential benefits of the new wing design in terms of improved aerodynamic performance and structural robustness, thereby contributing to the advancement of aerospace engineering... View More»
    DOI: 10.14303/2315-5663.2023.124

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