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风洞背景压力对声爆测量影响及抑制技术研究

杨洋 钱丰学 周波 豆帅威 高荣钊

空气动力学学报2026,Vol.44Issue(8):46-57,12.
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空气动力学学报2026,Vol.44Issue(8):46-57,12.DOI:10.7638/kqdlxxb-2025.0088

风洞背景压力对声爆测量影响及抑制技术研究

Research on the influence of wind tunnel background pressure interference effects on sonic boom measurement and its suppression techniques

杨洋 1钱丰学 1周波 1豆帅威 1高荣钊1

作者信息

  • 1. 中国空气动力研究与发展中心 高速空气动力研究所,绵阳 621000
  • 折叠

摘要

Abstract

Wind tunnel test is a crucial means for evaluating the low sonic boom characteristics of supersonic civil aircraft and validating related design prediction methods.Investigating the influence of wind tunnel background pressure(WBP)on sonic boom measurement and developing suppression techniques are essential for establishing reliable wind tunnel test methodologies for sonic boom measurement.This study focuses on the unique spatiotemporal distribution and coupling characteristics of WBP.Through theoretical analysis and experimental verification,the mechanism of its influence on sonic boom measurement is explored.The independent effects of WBP distribution in the time and spatial domains under approximate decoupling conditions are successfully revealed.A fine-control strategy for the settling chamber total pressure is proposed,which employs a composite control method combining feedforward and PID feedback to suppress temporal influences.This strategy improves the total pressure control accuracy from 0.2%~0.3%to better than 0.15%,significantly reducing the temporal non-uniformity of WBP.By integrating specific test arrangements,selecting the region with minimal fluctuations as the test section and applying spatial averaging data processing,a comprehensive strategy is formed.This effectively enhances the ability to distinguish and extract weak sonic boom signals in environments with high spatial disturbances.Applying this methodology to low sonic boom supersonic civil aircraft benchmark model tests in a 2 m supersonic wind tunnel shows that the near-field sonic boom measurement results are in good agreement with those obtained from continuous wind tunnels of similar scale internationally.The deviation of the head shock peak is less than 3%,validating the effectiveness of the proposed framework in mitigating the influence of wind tunnel background pressure on sonic boom measurement.

关键词

风洞试验/风洞背景压力/声爆测量/时域/空间域

Key words

wind tunnel test/wind tunnel background pressure(WBP)/sonic boom measurement/temporal domain/spatial domain

分类

航空航天

引用本文复制引用

杨洋,钱丰学,周波,豆帅威,高荣钊..风洞背景压力对声爆测量影响及抑制技术研究[J].空气动力学学报,2026,44(8):46-57,12.

基金项目

国家级项目 ()

空气动力学学报

0258-1825

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