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Abstract <p>Methods for reducing the shock wave produced by supersonic passenger aircraft are considered. Aerodynamic contouring of the aircraft to reduce the boom is proposed. A method is developed for assessing the proposed contours in the early design stages.</p>

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Shaping a Supersonic Passenger Aircraft with Minimal Sonic Boom

  • 期刊论文

  • 发表日期：

    2025年3月1日

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  • R. Kh. Arifullin,
  • S. A. Serebryanskiy,
  • S. N. Shkarubo

摘要

Abstract

Methods for reducing the shock wave produced by supersonic passenger aircraft are considered. Aerodynamic contouring of the aircraft to reduce the boom is proposed. A method is developed for assessing the proposed contours in the early design stages.