Year: 2025
Type: article
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.
Author: Satish Gupta
Institution: MVJ College of Engineering
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: hybrid
OpenAlex ID: W4409447811