共轴对转螺旋桨气动与噪声特性研究进展

刘沛清; 吕昌昊; 胡天翔; 屈秋林; 耿欣; 孙韬

doi:10.7638/kqdlxxb-2023.0054

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共轴对转螺旋桨气动与噪声特性研究进展

研究专栏——航空螺旋桨设计研究进展 | 更新时间：2026-05-28

- 共轴对转螺旋桨气动与噪声特性研究进展
- Review of aerodynamic and aeroacoustics characteristics of counter rotating propellers
- 空气动力学学报 2023年41卷第10期页码：100-125
- 作者机构：
  
  北京航空航天大学航空气动声学工信部重点实验室,北京,100191
- 作者简介：
  
  刘沛清（1960-），男，教授，博导，研究方向：空气动力学与气动声学. E-mail：lpq@buaa.edu.cn
  胡天翔*（1986-），男，副教授，研究方向：飞行器设计，空气动力学. E-mail：tianxiang.hu@buaa.edu.cn
- 基金信息：
- DOI：10.7638/kqdlxxb-2023.0054
  中图分类号： V211.44
- 纸质出版：2023
- 稿件说明：
移动端阅览
刘沛清, 吕昌昊, 胡天翔, 等. 共轴对转螺旋桨气动与噪声特性研究进展[J]. 空气动力学学报, 2023, 41(10): 100−125.

LIU Peiqing, LYU Changhao, HU Tianxiang, et al. Review of aerodynamic and aeroacoustics characteristics of counter rotating propellers[J]. 2023, 41(10): 100-125.
刘沛清, 吕昌昊, 胡天翔, 等. 共轴对转螺旋桨气动与噪声特性研究进展[J]. 空气动力学学报, 2023, 41(10): 100−125. DOI： 10.7638/kqdlxxb-2023.0054

LIU Peiqing, LYU Changhao, HU Tianxiang, et al. Review of aerodynamic and aeroacoustics characteristics of counter rotating propellers[J]. 2023, 41(10): 100-125. DOI： 10.7638/kqdlxxb-2023.0054.

摘要

共轴对转螺旋桨由于拉力大、气动效率高而备受人们的关注。本文从共轴对转螺旋桨的试验研究、气动性能评估、气动模拟、气动噪声预测、气动噪声优化设计等方面进行了综述。首先，总结了目前国内外在共轴对转螺旋桨气动及噪声方面的试验成果；随后，介绍了共轴对转螺旋桨气动力计算的工程方法，并详细阐述了北京航空航天大学陆士嘉实验室提出的共轴对转螺旋桨气动力评估的片条理论发展与参数选择；然后，介绍了共轴对转螺旋桨数值模拟方法，并针对共轴对转螺旋桨气动噪声预测的频域方法和时域方法进行了论述；最后，介绍了目前共轴对转螺旋桨气动噪声优化设计的研究成果。

Abstract

Counter rotating propellers (CRPs) have recently attracted more attention due to their high thrust and aerodynamic efficiency. This article comprehensively reviews five aspects of coaxial CRPs: experimental research

aerodynamic performance evaluation

aerodynamic simulation

aeroacoustics prediction

and aerodynamic noise optimization design. Firstly

it summarizes the current domestic and international experimental achievements regarding the aerodynamics and aeroacoustics of CRPs. Next

it introduces the engineering methods for the aerodynamic force calculation of CRPs and elaborates on the strip theory developed by Lu Shijia Laboratory at Beihang University for the aerodynamic force evaluation of CRPs. Based on this

numerical simulation methods for CRPs are presented

and both frequency domain and time domain methods for predicting the aerodynamic noise of CRPs are discussed. Finally

it presents the current research achievements in the aerodynamic noise optimization design of CRPs.

关键词

Keywords

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