螺旋桨气动参数与飞机综合设计技术

许正宇; 汤斯佳; 何淼; 昝丙合; 曹德松

doi:10.7638/kqdlxxb-2023.0046

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螺旋桨气动参数与飞机综合设计技术

研究专栏——航空螺旋桨设计研究进展 | 更新时间：2026-05-28

- 螺旋桨气动参数与飞机综合设计技术
- Research on propeller parameters and integrated design with aircraft
- 空气动力学学报 2023年41卷第10期页码：88-99
- 作者机构：
  
  1. 航空工业惠阳航空螺旋桨有限责任公司,保定,071052
  2. 河北省螺旋桨结构与动力性能重点实验室,保定,071052
  3. 北京航空航天大学航空科学与工程学院,北京,100191
  4. 空军装备部北京局驻保定地区军事代表室,保定,071000
- 作者简介：
  
  许正宇（1992-），河北保定人，设计员，研究方向：螺旋桨总体设计. E-mail：zhengyuxu@buaa.edu.cn
  昝丙合*（1985-），河北沧州人，高级工程师，研究方向：螺旋桨空气动力学. E-mail：zbh8800@163.com
- 基金信息：
  
  河北省螺旋桨结构与动力性能重点实验室支持项目（BPFKEP202204）
- DOI：10.7638/kqdlxxb-2023.0046
  中图分类号： V211.44
- 纸质出版：2023
- 稿件说明：
移动端阅览
许正宇, 汤斯佳, 何淼, 等. 螺旋桨气动参数与飞机综合设计技术[J]. 空气动力学学报, 2023, 41(10): 88−99.

XU Zhengyu, TANG Sijia, HE Miao, et al. Research on propeller parameters and integrated design with aircraft[J]. 2023, 41(10): 88-99.
许正宇, 汤斯佳, 何淼, 等. 螺旋桨气动参数与飞机综合设计技术[J]. 空气动力学学报, 2023, 41(10): 88−99. DOI： 10.7638/kqdlxxb-2023.0046

XU Zhengyu, TANG Sijia, HE Miao, et al. Research on propeller parameters and integrated design with aircraft[J]. 2023, 41(10): 88-99. DOI： 10.7638/kqdlxxb-2023.0046.

摘要

螺旋桨推进具备较高的推进效率和广泛的通用性。由于桨盘面积大、滑流范围广，螺旋桨与载机间的空气动力耦合关系更加紧密，需要将螺旋桨与飞机进行综合设计，迭代获取优化设计方案，从而最大化保证飞机的高性能和经济性。本文首先介绍了飞机总体设计对螺旋桨气动设计参数的影响，以及螺旋桨多目标优化综合设计的手段；然后，简述了螺旋桨布局选型对飞机总体设计的影响，介绍了共轴对转螺旋桨设计和分布式推进螺旋桨设计两种新形态的螺旋桨设计构型；最后，讨论了螺旋桨设计手段的发展，以及CFD方法在螺旋桨-飞机综合设计中的应用。本文可为螺旋桨飞机的相关总体设计和气动优化提供参考。

Abstract

For aircraft

propellers have higher efficiency than other forms of propulsion and demonstrate wide-range versatility. The close aerodynamic coupling between the propeller and aircraft fuselage necessitates a comprehensive design of propeller-driven aircraft for better performance. This paper first introduces the requirements of aircraft design for propellers

such as but not limited to their diameters

blade numbers

and airfoil configurations

accompanied by the multidisciplinary optimizing design methods for propellers. Then

it examines the ramifications of propeller layout on aircraft design

focusing on two novel propeller configurations: co-axial counter-rotating propellers and distributed propellers. Furthermore

the evolution of propeller design techniques is traced

and the application of Computational Fluid Dynamics (CFD) in computational aeroacoustics

three-dimensional shape optimization

evaluation of aerodynamic interference

and comprehensive aircraft design is summarized. This paper will serve as a valuable reference for designing and optimizing propeller-driven aircraft.

关键词

Keywords

references

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