Progress in hypersonic boundary layer transition delay control

被引：0
作者：
Liu Q. [1 ,2 ]
Tu G. [1 ]
Luo Z. [2 ]
Chen J. [1 ]
Zhao R. [3 ]
Yuan X. [1 ]
机构：
[1] State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang
[2] College of Aerospace Science and Engineering, National University of Defense Technology, Changsha
[3] School of Aerospace Engineering, Beijing Institute of Technology, Beijing
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2022年 / 43卷 / 07期
基金：
中国国家自然科学基金;
关键词：
boundary layer transition; drag and heat reduction; flow control; hypersonic flight vehicles; transition delay;
D O I：
10.7527/S1000-6893.2021.25357
中图分类号：
学科分类号：
摘要：
Due to the large difference between laminar flow and turbulent flow in wall friction and wall heat flow, the transition control of the hypersonic boundary layer is of vital importance to the aerodynamic performance and thermal protection system of vehicles. This paper first summarizes the main instability mechanisms of hypersonic boundary layers, followed by a review of the latest progress in the hypersonic boundary layer transition delay control technology from two aspects, namely, passive control and active control technologies. Passive control methods such as roughness elements, wavy wall, and porous coating are then introduced in detail, the active control measures such as wall heating/cooling and heavy gas injection described, the physical mechanism behind the control analyzed, and the advantages and disadvantages of various control technologies discussed. Finally, suggestions and prospects for further research on transition delay control are presented. © 2022 AAAS Press of Chinese Society of Aeronautics and Astronautics. All rights reserved.
引用
收藏
相关论文
共 114 条
[1]  
ZHEN H P, JIANG C W., Review of hypersonic flight validation vehicles-HTV-2, Aerodynamic Missile Journal, 6, pp. 7-13, (2013)
[2]  
ZHOU H, ZHANG H X., Two problems in the transition and turbulence for near space hypersonic flying vehicles [J], Acta Aerodynamica Sinica, 35, 2, pp. 151-155, (2017)
[3]  
YU P, DUAN Y, CHEN J., Some aerodynamic issues in hypersonic flight [J], Acta Aeronautica et Astronautica Sinica, 36, 1, pp. 7-23, (2015)
[4]  
SLOTNICK J, KHODADOUST A, ALONSO J, Et al., CFD vision 2030 study: A path to revolutionary computational aerosciences: NASA/CR-2014-218178, (2014)
[5]  
LIU Q, LUO Z B, WANG L, Et al., Direct numerical simulations of supersonic turbulent boundary layer with stre-amwise-striped wall blowing, Aerospace Science and Technology, 110, (2021)
[6]  
BERTIN J J, CUMMINGS R M., Critical hypersonic aero-thermodynamic phenomena, Annual Review of Fluid Mechanics, 38, pp. 129-157, (2006)
[7]  
WHITEHEAD A., NASP aerodynamics: AIAA-1989-5013, (1989)
[8]  
SCHNEIDER S P., Developing mechanism-based methods for estimating hypersonic boundary-layer transition in flight: the role of quiet tunnels, Progress in Aerospace Sciences, 72, pp. 17-29, (2015)
[9]  
LUO J S., Transition and prediction for hypersonic boundary layers [J], Acta Aeronautica et Astronautica Sinica, 36, 1, pp. 357-372, (2015)
[10]  
CHEN J Q, TU G H, ZHANG Y F, Et al., Hypersnonic boundary layer transition: What we know, where shall we go [J], Acta Aerodynamica Sinica, 35, 3, pp. 311-337, (2017)
12345678910