International Journal For Multidisciplinary Research

E-ISSN: 2582-2160   •   Impact Factor: 9.24

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A Newer Approach to Aerodynamic Design of Wings for Wide Range of Mach number Application

Author(s) Prof. Satish Chander Gupta
Country India
Abstract A flat surface wing is optimized for minimum induced drag for a high subsonic Mach number. Wing for transport airplane role is considered.Optimal warp is separated into twist and camber. Angle-of-attack is alleviated by the value of twist at root, and the optimal warp is reduced by this value. Now aerofoil thickness is superimposed and the 3-D aerofoils so generated are analysed for transonic flow through finite difference methodology.
Keywords Induced drag,optimal warp,twist,camber, transonic flow analysis
Field Engineering
Published In Volume 7, Issue 2, March-April 2025
Published On 2025-04-14
DOI https://doi.org/10.36948/ijfmr.2025.v07i02.39416
Short DOI https://doi.org/g9fm5c
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