Research status and development tendency of large aircraft wind tunnel technologies in China

WU Junqiang; CUI Xiaochun; WEI Zhi; DU Wentian

doi:10.7638/kqdlxxb-2023.0147

English Version Journal Login

您当前的位置：

首页 >

文章列表页 >

Research status and development tendency of large aircraft wind tunnel technologies in China

更新时间：2026-05-28

- Research status and development tendency of large aircraft wind tunnel technologies in China
- Vol. 41, Issue 12, Pages: 83-94(2023)
- 作者机构：
  
  1. 中国空气动力研究与发展中心,绵阳,621000
  2. 中国航空工业空气动力研究院,沈阳,110034
  3. 高速高雷诺数气动力航空科技重点实验室,沈阳,110034
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2023.0147
  CLC： V211.71
- Published：2023
- 稿件说明：
移动端阅览
吴军强, 崔晓春, 魏志, 等. 我国大型飞机风洞试验技术研究现状与发展趋势[J]. 空气动力学学报, 2023, 41(12): 83−94.

WU Junqiang, CUI Xiaochun, WEI Zhi, et al. Research status and development tendency of large aircraft wind tunnel technologies in China[J]. 2023, 41(12): 83-94.
吴军强, 崔晓春, 魏志, 等. 我国大型飞机风洞试验技术研究现状与发展趋势[J]. 空气动力学学报, 2023, 41(12): 83−94. DOI： 10.7638/kqdlxxb-2023.0147

WU Junqiang, CUI Xiaochun, WEI Zhi, et al. Research status and development tendency of large aircraft wind tunnel technologies in China[J]. 2023, 41(12): 83-94. DOI： 10.7638/kqdlxxb-2023.0147.

摘要

大型飞机风洞试验技术是大型飞机产业化发展的重要技术基础。本文简要介绍了大型飞机气动布局特点及其风洞试验需求，阐述了近十多年来我国在边界层转捩精确模拟与流动精细化观测、高速风洞试验模型支撑、精细化气动力/气动载荷测量、气动力试验数据修正、气动噪声、结冰与防除冰等大型飞机风洞试验技术研究方面的发展现状，分析了我国现有风洞试验技术能力水平与航空发达国家及未来型号发展需要之间的差距，并提出了下一步发展建议。

Abstract

Large wind tunnels and related test techniques are indispensible foundation for the development of large aircraft. This article briefly introduces the aerodynamic characteristics of large aircraft and their wind tunnel test requirements. It also elaborates on the research status of large wind tunnel test techniques in China in the past decade

including the accurate simulation of boundary layer transition

flow field visualization

high-speed wind tunnel test model support

fine aerodynamic force/aerodynamic load measurement

aerodynamic force test data correction

aerodynamic noise

ice formation and deicing. It analyzes the gap between China's current wind tunnel test technology ability level and the needs of aviation developed countries and future model development

and puts forward development suggestions for the next step.

关键词

Keywords

references

CHEN D H, LIN J, GUO D P, et al . Technical ways to solve high speed key aerodynamic problems of large air transporters[J ] . Experiments and Measurements in Fluid Mechanics, 2004 , 18 ( 2 ): 1 − 5 (in Chinese).

ZHAN P G. Overseas wind tunnel testing[M]. Beijing: National Defense Industry Press, 2018(in Chinese).

NI Z S, LIU S Y, WANG Q, et al . Research progress of test technologies for 3 m × 2 m icing wind tunnel[J ] . Journal of Experiments in Fluid Mechanics, 2019 , 33 ( 6 ): 46 − 53 (in Chinese).

FAN J C, YU T . Low speed pressurized wind tunnel at home which is building[J ] . Journal of Experiments in Fluid Mechanics, 2005 , 19 ( 3 ): 1 − 6 (in Chinese).

LIU P Q, GUO H . Research progress of aeroacoustics wind tunnel experiments in Beihang LU Shijia laboratory[J ] . Civil Aircraft Design Research, 2022 ( 1 ): 1 − 23 (in Chinese).

LI Z F. Handbook of wind tunnel test[M]. Beijing: Aviation Industry Press, 2015(in Chinese).

WANG M, LI Y J, ZHAO R H, et al . Transition detection technique for wide speed range by means of on-line heating coating[J ] . Acta Aeronautica et Astronautica Sinica, 2022 , 43 ( 11 ): 190 − 199 (in Chinese).

ZHANG Z Y, WANG X S, HUANG X H, et al . Videogrammetry measurement for high-speed complex flow structures[J ] . Acta Aeronautica et Astronautica Sinica, 2017 , 38 ( 8 ): 120989 (in Chinese).

CHEN D H, LIU D W, YIN L P, et al . The study of versatile support system in the 2.4 m transonic wind tunnel[J ] . Journal of Experiments in Fluid Mechanics, 2013 , 27 ( 3 ): 98 − 102,112 (in Chinese).

ZHANG Z Y, HUANG X H, YIN J, et al . Research status and application of videogrammetric measurement techniques for wind tunnel testing[J ] . Acta Aerodynamica Sinica, 2016 , 34 ( 1 ): 70 − 79 (in Chinese).

WEI Z, XIE Y, WU J Q, et al . Application of continuous sweeping force measuring technology in large intermittent transonic wind tunnel[J ] . Journal of Experiments in Fluid Mechanics, 2011 , 25 ( 4 ): 99 − 102 (in Chinese).

XIE Y, LI P, JIANG H, et al . Research on key technologies of continuous variable angle of attack test in 2.4 m transonic wind tunnel[J ] . Journal of Experiments in Fluid Mechanics, 2014 , 28 ( 1 ): 89 − 93 (in Chinese).

XIONG J, LI G S, ZHOU Q, et al . Development and application of pressure sensitive paint system in 2.4 m transonic wind tunnel[J ] . Journal of Experiments in Fluid Mechanics, 2016 , 30 ( 3 ): 76 − 84 (in Chinese).

LI G S, ZHOU Q, MA H S, et al . Image processing methods of pressure sen sitive paint based on prior calibration[J ] . Acta Aerodynamica Sinica, 2014 , 32 ( 2 ): 197 − 202 (in Chinese).

LI G S, ZHOU Q, LIU X, et al . Experimental research of pressure sensitive paint performance and calibration technique[J ] . Acta Aeronautica et Astronautica Sinica, 2013 , 34 ( 2 ): 227 − 234 (in Chinese).

SHANG J K, LI Y J, ZHAO H Y, et al. Integrated application research of PIV and PSP technology in large aircraft wind tunnel Test[J ] . Acta Aerodynamica Sinica, 2023, 41(11): 107 − 117 (in Chinese).

MA Y M, AI M Q, ZHANG Y J, et al . Experimental investigation on the effects of skin waviness and step-height based on RVSM operation requirement[J ] . Aerodynamic Research Experiment, 2023 , 01 ( 02 ): 118 − 126 (in Chinese).

ZHOU X, YANG S P, ZHONG Y . Study on aerodynamic design of static pressure source based on RVSM performance requirements of civil aircraft[J ] . Machine Design and Manufacturing Engineering, 2022 , 51 ( 4 ): 54 − 58 (in Chinese).

LIU D W, XIONG G T, LIU Y, et al . Method of test data correction for wide-body aircraft in high speed wind tunnel[J ] . Acta Aeronautica et Astronautica Sinica, 2019 , 40 ( 2 ): 522205 (in Chinese).

LIU D W, CHEN D H, YIN L P, et al . Investigation on the vane cable suspension support system in the 2.4 m Transonic Wind Tunnel[J ] . Acta Aerodynamica Sinica, 2016 , 34 ( 3 ): 354 − 361 (in Chinese).

LIU G Y, WEI Z, PENG X, et al . Application of slotted wall interference assessment and correction technique in transonic wind tunnel[J ] . Acta Aeronautica et Astronautica Sinica, 2018 , 39 ( 2 ): 121499 − 121499 (in Chinese).

GUO Q T, SUN Y, GUO Z, et al . Separation method for Reynolds number/static aeroelastic coupling effect in wind tunnel test[J ] . Acta Aeronautica et Astronautica Sinica, 2022 , 43 ( 11 ): 452 − 462 (in Chinese).

CHEN B, LI Z F, ZHOU G C, et al . Experimental technology research on airframe noise in large scale aero-acoustic wind tunnel[J ] . Aerodynamic Research Experiment, 2023 , 1 ( 5 ): 71 − 79 (in Chinese).

LIU S Y, WANG Q, YI X, et al . New progress of 3 m × 2 m icing wind tunnel test technology from 2020 to 2022[J ] . Acta Aerodynamica Sinica, 2023 , 41 ( 1 ): 57 − 65 (in Chinese).

LAI Q R, LIU Q L, GUO L, et al . Icing and anti-icing test technology of aero-engine based on large-scale icing wind tunnel[J ] . Journal of Experiments in Fluid Mechanics, 2021 , 35 ( 3 ): 1 − 8 (in Chinese).

ZHU D Y, PEI R N, YANG Q M, et al . Experimental research on a hot air anti-icing system in FL-61 icing wind tunnel[J ] . Aerodynamic Research Experiment, 2023 , 1 ( 5 ): 107 − 112 (in Chinese).

PEI R N, ZHU D Y, SHU J . Icing test of characteristic of runback ice accretions on horizontal tail[J ] . Journal of Nanjing University of Aeronautics Astronautics, 2022 , 54 ( 6 ): 1074 − 1082 (in Chinese).

YU L, WU Y A, ZHAO H Y, et al . A study on the sensitivities of an ice protection system combining thermoelectric and superhydrophobic coating to icing environment parameters[J ] . Applied Sciences, 2023 , 13 ( 11 ): 6607 .

ZHU D Y, FENG Q, HAN X T, et al . Researches on a large natural moveable icing wind tunnel and test methods[J ] . Journal of Experiments in Fluid Mechanics, 2022 , 36 ( 1 ): 52 − 61 (in Chinese).

ZHENG L, PENG Y X, BU X Q, et al . Parameter measurement method and physical meteorology simulation for designing anti-icing system of aircraft[J ] . Science Technology Review, 2013 , 31 ( 25 ): 26 − 31 (in Chinese).

Views

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

The correlation between the running pressure ratio and state parameters in a cryogenic transonic wind tunnel

The study of interference characteristics of typical support struts on large aircraft in high-speed wind tunnels

Numerical and experimental study on aerodynamic design for the rear wing of an electric sports car

Noise prediction and reduction methods for LAGOON landing gear based on Lattice Boltzmann method

An Ac-criteria-based optimal input design method

Related Author

HUANG Zhilong

WANG Ning

LIAO Daxiong

LI Qiang

LIU Dawei

XU Xin

CHEN Dehua

WEI Zhi

Related Institution

Key Laboratory of Unsteady Aerodynamics and Flow Control, Nanjing University of Aeronautics and Astronautics, Nanjing

Facility Design and Instrumentation Institute, China Aerodynamics Research and Development Center, Mianyang

State Key Laboratory of Aerodynamics

High Speed Aerodynamics Institute of China Aerodynamics Research and Development Center

AI问答

⁰