Progress and challenges of sonic boom research

QIAN Zhansen; HAN Zhonghua

doi:10.7638/kqdlxxb-2019.0054

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Progress and challenges of sonic boom research

更新时间：2026-05-28

- Progress and challenges of sonic boom research
- Vol. 37, Issue 4, Pages: 601-619(2019)
- 作者机构：
  
  1. 中国航空工业空气动力研究院,沈阳,110034
  2. 高速高雷诺数气动力航空科技重点实验室,沈阳,110034
  3. 西北工业大学航空学院超声速客机研究中心,西安,710072
  4. 西北工业大学航空学院气动与多学科优化设计研究所,西安,710072
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2019.0054
  CLC： V211.7
- Published：2019
- 稿件说明：
移动端阅览
钱战森, 韩忠华. 声爆研究的现状与挑战[J]. 空气动力学学报, 2019, 37(4): 601-619.

QIAN Zhansen, HAN Zhonghua. Progress and challenges of sonic boom research[J]. 2019, 37(4): 601-619.
钱战森, 韩忠华. 声爆研究的现状与挑战[J]. 空气动力学学报, 2019, 37(4): 601-619. DOI： 10.7638/kqdlxxb-2019.0054.

QIAN Zhansen, HAN Zhonghua. Progress and challenges of sonic boom research[J]. 2019, 37(4): 601-619. DOI： 10.7638/kqdlxxb-2019.0054.

摘要

声爆是超声速飞行器所特有的一种气动声学现象，其涉及空气动力学和非线性声学等研究领域，开展相关研究具有重要的学术意义和应用前景。本文简述了声爆的基本概念、主要特征和主要危害，简要回顾了声爆的产生、发展和演化的研究历史，重点介绍了声爆的数值模拟、风洞试验和飞行试验预测方法，以及近年来提出的声爆抑制方法和低声爆气动优化设计方法的发展现状；最后总结了当前声爆预测方法面临的技术难点和挑战。

Abstract

Sonic boom is a special aero-acoustic phenomenon for supersonic aircraft

which contains both the fields of aerodynamics and nonlinear acoustics

so it is of important academic significance and application prospect. The present paper introduces its basic conception and major characteristics

the research history of its generation

development and evolution

and its harmfulness; Then the numerical simulation method

wind tunnel experiment method and flight test method of sonic boom researches are emphatically presented

and also including the recently proposed sonic boom inhibition and low boom optimization design methods; Finally

the current technique difficulties and challenges of sonic boom prediction are summarized.

关键词

Keywords

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