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Abstract <p>A method is proposed for optimizing the aerodynamic layout of a supersonic passenger aircraft in order to reduce the drag force and intensity of the sonic boom. In the process of searching for the optimal solution with a fixed lift coefficient, the wing twist, the shape of the centerline, and the V-angle of the wing are varied. The wing planform and its volume remain unchanged. Examples of optimizing the test aerodynamic layout in a wing-plus-fuselage configuration are presented.</p>

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Optimization Method for the Aerodynamic Layout of a Supersonic Passenger Aircraft with the Aim of Reducing the Drag Force and Sonic Boom

  • 期刊论文

  • 发表日期：

    2025年8月31日

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  • A. V. Wolkov,
  • U. G. Ibragimov,
  • O. V. Karas,
  • M. A. Meniailov,
  • I. L. Chernyshyov

摘要

Abstract

A method is proposed for optimizing the aerodynamic layout of a supersonic passenger aircraft in order to reduce the drag force and intensity of the sonic boom. In the process of searching for the optimal solution with a fixed lift coefficient, the wing twist, the shape of the centerline, and the V-angle of the wing are varied. The wing planform and its volume remain unchanged. Examples of optimizing the test aerodynamic layout in a wing-plus-fuselage configuration are presented.