可压缩湍流边界层燃烧减阻研究综述

刘宏鹏; 高振勋; 蒋崇文; 李椿萱

doi:10.7638/kqdlxxb-2019.0147

欢迎来到能源电力期刊网！

English Version 期刊登录

您当前的位置：

首页 >

文章列表页 >

可压缩湍流边界层燃烧减阻研究综述

专栏——湍流燃烧 | 更新时间：2026-05-28

- 可压缩湍流边界层燃烧减阻研究综述
- Review of researches on compressible turbulent boundary layer combustion for skin friction reduction
- 空气动力学学报 2020年38卷第3期页码：593-602
- 作者机构：
  
  北京航空航天大学航空科学与工程学院,北京,100191
- 作者简介：
  
  刘宏鹏(1992-), 男, 湖南人, 博士研究生, 研究方向:高超声速空气动力学.E-mail:hpliu@buaa.edu.cn
  高振勋(1982-), 副教授, 研究方向:高超声速空气动力学.E-mail:gaozhenxun@buaa.edu.cn
- 基金信息：
  
  国家自然科学基金重大研究计划面上项目(91641123)
- DOI：10.7638/kqdlxxb-2019.0147
  中图分类号： V211.3;TK16
- 纸质出版：2020
- 稿件说明：
移动端阅览
刘宏鹏, 高振勋, 蒋崇文, 李椿萱. 可压缩湍流边界层燃烧减阻研究综述[J]. 空气动力学学报, 2020, 38(3): 593-602.

LIU Hongpeng, GAO Zhenxun, JIANG Chongwen, et al. Review of researches on compressible turbulent boundary layer combustion for skin friction reduction[J]. 2020, 38(3): 593-602.
刘宏鹏, 高振勋, 蒋崇文, 李椿萱. 可压缩湍流边界层燃烧减阻研究综述[J]. 空气动力学学报, 2020, 38(3): 593-602. DOI： 10.7638/kqdlxxb-2019.0147.

LIU Hongpeng, GAO Zhenxun, JIANG Chongwen, et al. Review of researches on compressible turbulent boundary layer combustion for skin friction reduction[J]. 2020, 38(3): 593-602. DOI： 10.7638/kqdlxxb-2019.0147.

摘要

减阻设计对于提高超燃冲压发动机性能具有重要意义，而边界层燃烧是一种有效的减阻方法。综述分别从实验、理论和数值模拟研究方面介绍了边界层燃烧减阻的相关进展。实验研究验证了边界层燃烧减阻的有效性，研究了不同因素对边界层燃烧减阻效率的影响，初步形成了将该减阻技术应用于高超声速飞行器的能力。理论研究建立了考虑边界层燃烧的壁面摩阻、热流理论计算模型，而数值模拟帮助揭示了边界层燃烧减阻的内在物理机理。澳大利亚Queensland大学在该方面开展了较为系统的研究，欧洲、美国、俄罗斯、日本等在该方面极少公开发表相关研究成果。中国学者取得了一定进展，但与世界先进水平仍有较大差距，尤其是在实验研究方面。

Abstract

Drag reduction is important for improving the performance of scramjet engines operating at high Mach numbers. One demonstrated method for reducing skin friction drag on a surface exposed to hypersonic flow is the injection and combustion of hydrogen fuel in the boundary layer. This paper reviews the research progresses of skin friction reduction by boundary layer combustion from three aspects including experiments

theory analyses

and numerical simulations. The experiments have demonstrated their effectiveness and analyzed different influencing factors. The ability of applying this drag reduction technique to real hypersonic flight vehicles is primarily established. The theoretical prediction model for skin friction and heat flux of the boundary layer flow where the combustion occurs has been proposed and its accuracy was demonstrated by comparing with experiments and numerical studies. The numerical simulations have helped researchers to understand the mechanism of skin friction reduction by boundary layer combustion deeply. For the research progresses of this technique

University of Queensland in Australia is at the leading level of the world. Europe

America

Russia and Japan seem having little interest on this field and very few technical papers can be found publicly from these countries. While Chinese researchers has made some progresses but still need to do lots of work

epspcially in the experimental field

to catch up with the world leading level.

关键词

Keywords

references

FRY R S. A century of ramjet propulsion technology evolution[J]. Journal of Propulsion and Power, 2004, 20(1):27-58. https://doi.org/10.2514/1.9178

DENMAN A. Large eddy simulation of compressible turbulent boundary layers with heat addition[D]. Australia: University of Queensland, 2007.

KIRCHHARTZ R M, MEE D J, STALKER R J. Supersonic skin-friction drag with tangential wall slot fuel injection and combustion[J]. AIAA Journal, 2012, 50(2):313-324. https://doi.org/10.2514/1.j051073

LI K W, LIAN Q X. A review on drag reduction of boundary layer[J]. Journal of Beijing University of Aeronautics and Astronautics, 1991, 17(4):68-76. (in Chinese)

COUSTOLS E. Control of turbulent flows for skin friction drag reduction[M]//Control of Flow Instabilities and Unsteady Flows. Vienna:Springer Vienna, 1996:155-202. https://doi.org/10.1007/978-3-7091-2688-2_4

BUSHNELL D, HEFNER J. Viscous drag reduction in boundary layers[M ] //SEEBASS A R.Progress in Astronautics and Aeronautics. Washington DC: AIAA, 1990. https://doi.org/10.2514/4.865978

WALSH M J, WEINSTEIN L M. Drag and heat transfer on surfaces with small longitudinal fins[C ] //11th Fluid and Plasma Dynamics Conference, Seattle, WA, USA. Reston, Virigina: AIAA, 1978: https://doi.org/10.2514/6.1978-1161

WALSH M J. Riblets as a viscous drag reduction technique[J]. AIAA Journal, 1983, 21(4):485-486. https://doi.org/10.2514/3.60126

SAREEN A, DETERS R, HENRY S, et al. Drag reduction using riblet film applied to airfoils for wind turbines[C ] //49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, Florida. Reston, Virigina: AIAA. AIAA 2011-558. https://doi.org/10.2514/6.2011-558

ANTONIA R A, ZHU Y, SOKOLOV M. Effect of concentrated wall suction on a turbulent boundary layer[J]. Physics of Fluids, 1995, 7(10):2465-2474. https://doi.org/10.1063/1.868690

PARK J, CHOI H. Effects of uniform blowing or suction from a spanwise slot on a turbulent boundary layer flow[J]. Physics of Fluids, 1999, 11(10):3095-3105. https://doi.org/10.1063/1.870167

CHUNG Y M, SUNG H J, KROGSTAD P A. Modulation of near-wall turbulence structure with wall blowing and suction[J]. AIAA Journal, 2002, 40(8):1529-1535. https://doi.org/10.2514/2.1849

OYEWOLA O M. Streamwise variations of higher-order turbulence statistics in a turbulent boundary layer subjected to localise wall suction[J]. International Journal of Mechanical Sciences, 2006, 48(10):1163-1171. https://doi.org/10.1016/j.ijmecsci.2006.04.001

SIMPSON R L. Characteristics of turbulent boundary layers at low Reynolds numbers with and without transpiration[J]. Journal of Fluid Mechanics, 1970, 42(4):769-802. https://doi.org/10.1017/s002211207000160x

WILKINSON S P.. Influence of wall permeability on turbulent boundary-layer properties[C ] //21st Aerospace Sciences Meeting, Reno, NV, USA. Reston, Virigina: AIAA, 1983. https://doi.org/10.2514/6.1983-294

DERSHIN H, LEONARD C A, GALLAHER W H. Direct measurement of skin friction on a porous flat plate with mass injection[J]. AIAA Journal, 1967, 5(11):1934-1939. https://doi.org/10.2514/3.4343

HWANG D. Review of research into the concept of the microblowing technique for turbulent skin friction reduction[J]. Progress in Aerospace Sciences, 2004, 40(8):559-575. https://doi.org/10.1016/j.paerosci.2005.01.002

PARTHASARATHY K, ZAKKAY V. An experimental investigation of turbulent slot injection at Mach 6[J]. AIAA Journal, 1970, 8(7):1302-1307. https://doi.org/10.2514/3.5889

SCHETZ J A, VANOVEREEM J. Skin friction reduction by injection through combinations of slots and porous sections[J]. AIAA Journal, 1975, 13(8):971-972. https://doi.org/10.2514/3.60492

CARY A M, HEFNER J N. Film-cooling effectiveness and skin friction in hypersonic turbulent flow[J]. AIAA Journal, 1972, 10(9):1188-1193. https://doi.org/10.2514/3.50348

RICHARDS B E, STOLLERY J L. Laminar film cooling experiments in hypersonic flow[J]. Journal of Aircraft, 1979, 16(3):177-181. https://doi.org/10.2514/3.58502

O'ONNOR J P, HAJI-SHEIKH A. Numerical study of film cooling in supersonic flow[J]. AIAA Journal, 1992, 30(10):2426-2433. https://doi.org/10.2514/3.11243

JUHANY K A, HUNT M L, SIVO J M. Influence of injectant Mach number and temperature on supersonic film cooling[J]. Journal of Thermophysics and Heat Transfer, 1994, 8(1):59-67. https://doi.org/10.2514/3.501

AUPOIX B, MIGNOSI A, VIALA S, et al. Experimental and numerical study of supersonic film cooling[J]. AIAA Journal, 1998, 36:915-923. https://doi.org/10.2514/3.13913

DELLIMORE K H, MARSHALL A W, CADOU C P. Influence of compressibility on film-cooling performance[J]. Journal of Thermophysics and Heat Transfer, 2010, 24(3):506-515. https://doi.org/10.2514/1.45092

GOYNE C P, STALKER R J, PAULL A, et al. Hypervelocity skin-friction reduction by boundary-layer combustion of hydrogen[J]. Journal of Spacecraft and Rockets, 2000, 37(6):740-746. https://doi.org/10.2514/2.3645

SWITHENBANK J, EAMES I, CHIN S, et al. Turbulent mixing in supersonic combustion systems[C ] //27th Aerospace Sciences Meeting, Reno, NV, USA. Reston, Virigina: AIAA. AIAA 89-0260. https://doi.org/10.2514/6.1989-260

BILLIG F S. Research on supersonic combustion[J]. Journal of Propulsion and Power, 1993, 9(4):499-514. https://doi.org/10.2514/3.23652

SURAWEERA M, MEE D, STALKER R. Skin friction reduction in hypersonic turbulent flow by boundary layer combustion[C]//43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada. Reston, Virigina: AIAA. AIAA-2005-0613. https: //doi.org/10.2514/6.2005-613

SURAWEERA M, et al. Reduction of skin friction drag in hypersonic flow by boundary layer combustion[D]. University of Queensland, 2006.

KIRCHHARTZ R M, MEE D J, STALKER R J. Supersonic skin-friction drag with tangential wall slot fuel injection and combustion[J]. AIAA Journal, 2012, 50(2):313-324. https://doi.org/10.2514/1.j051073

CHAN W Y K, MEE D J, SMART M K, et al. Drag reduction by boundary-layer combustion:effects of flow disturbances from rectangular-to-elliptical-shape-transition inlets[J]. Journal of Propulsion and Power, 2015, 31(5):1256-1267. https://doi.org/10.2514/1.b35335

KIRCHHARTZ R M, MEE D J, STALKER R J, et al. Supersonic boundary-layer combustion:effects of upstream entropy and shear-layer thickness[J]. Journal of Propulsion and Power, 2010, 26(1):57-66. https://doi.org/10.2514/1.44485

KIRCHHARTZ R M. Upstream wall layer effects on drag reduction with boundary layer combustion[D]. University of Queensland, 2010.

HOPKINS E J, INOUYE M. An evaluation of theories for predicting turbulent skin friction and heat transfer on flat plates at supersonic and hypersonic Mach numbers[J]. AIAA Journal, 1971, 9(6):993-1003. https://doi.org/10.2514/3.6323

BRADSHAW P. Compressible turbulent shear layers[J]. Annual Review of Fluid Mechanics, 1977, 9(1):33-52. https://doi.org/10.1146/annurev.fl.09.010177.000341

VAN DRIEST E R. Turbulent boundary layer in compressible fluids[J]. Journal of the Aeronautical Sciences, 1951, 18(3):145-160. https://doi.org/10.2514/8.1895

Van DRIEST E R. The problem of aerodynamic heating[J]. Aeronautical Engineering Review, 1956, 15(10):26-41.

STOLLERY J L. Supersonic turbulent boundary layers:some comparisons between experiment and a simple theory[J]. Aeronautical Quarterly, 1976, 27(2):87-98. https://doi.org/10.1017/s0001925900007599

SPALDING D B, CHI S W. The drag of a compressible turbulent boundary layer on a smooth flat plate with and without heat transfer[J]. Journal of Fluid Mechanics, 1964, 18(1):117-143. https://doi.org/10.1017/s0022112064000088

GOYNE C P, STALKER R J, PAULL A. Skin-friction measurements in high-enthalpy hypersonic boundary layers[J]. Journal of Fluid Mechanics, 2003, 485:1-32. https://doi.org/10.1017/s0022112003003975

STALKER R J. Control of hypersonic turbulent skin friction by boundary- layer combustion of hydrogen[J]. Journal of Spacecraft and Rockets, 2005, 42(4):577-587. https://doi.org/10.2514/1.8699

BARTH J E, WHEATLEY V, SMART M K. Hypersonic turbulent boundary-layer fuel injection and combustion:skin-friction reduction mechanisms[J]. AIAA Journal, 2013, 51(9):2147-2157. https://doi.org/10.2514/1.j052041

LIU H P, GAO Z X, TANG Y H, et al. Improvement of skin friction and heat transfer prediction theory of turbulent boundary-layer combustion of hydrogen[J]. International Journal of Hydrogen Energy, 2017, 42(41):26123-26131. https://doi.org/10.1016/j.ijhydene.2017.08.144

GAO Z X, JIANG C W, PAN S W, et al. Combustion heat-release effects on supersonic compressible turbulent boundary layers[J]. AIAA Journal, 2015, 53(7):1949-1968. https://doi.org/10.2514/1.j053585

CLARK R J, BADE SHRESTHA S O. Boundary layer combustion for skin friction drag reduction in scramjet combustors[C ] //50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, OH. Reston, Virginia: AIAA. AIAA-2014-3667. https://doi.org/10.2514/6.2014-3667

LUO K H. Combustion effects on turbulence in a partially premixed supersonic diffusion flame[J]. Combustion and Flame, 1999, 119(4):417-435. https://doi.org/10.1016/S0010-2180(99)00074-7

MAHLE I, FOYSI H, SARKAR S, et al. On the turbulence structure in inert and reacting compressible mixing layers[J]. Journal of Fluid Mechanics, 2007, 593:171-180. https://doi.org/10.1017/s0022112007008919

KNAUS R, PANTANO C. On the effect of heat release in turbulence spectra of non-premixed reacting shear layers[J]. Journal of Fluid Mechanics, 2009, 626:67-109. https://doi.org/10.1017/s0022112008005636

FERRER P J M, LEHNASCH G, MURA A. Compressibility and heat release effects in high-speed reactive mixing layers Ⅰ.:Growth rates and turbulence characteristics[J]. Combustion and Flame, 2017, 180:284-303. https://doi.org/10.1016/j.combustflame.2016.09.008

FERRER P J M, LEHNASCH G, MURA A. Compressibility and heat release effects in high-speed reactive mixing layers Ⅱ. Structure of the stabilization zone and modeling issues relevant to turbulent combustion in supersonic flows[J]. Combustion and Flame, 2017, 180:304-320. https://doi.org/10.1016/j.combustflame.2016.09.009

MENON S, FERNANDO E. A numerical study of mixing and chemical heat release in supersonic mixing layers[C]//28th Aerospace Sciences Meeting, Reno, NV, USA. Reston, Virigina: AIAA. AIAA 1990-0152. https: //doi.org/10.2514/6.1990-152

JR CALHOON W H ARUNAJATESAN S, DASH S M. Heat release and compressibility effects on planar shear layer development[C]//41st Aerospace Sciences Meeting and Exhibit, Reno, Nevada. Reston, Virigina: AIAA, 2003. AIAA 2003-1273. https: //doi.org/10.2514/6.2003-1273.

MIAO W B, CHENG X L, WANG Q. Analysis of the energy release effects in supersonic reacting flows[J]. Acta Aerodynamica Sinica, 2008, 26(3):339-343. (in Chinese)

LIU H P, GAO Z X, JIANG C W, et al. Numerical study of combustion effects on the development of supersonic turbulent mixing layer flows with WENO schemes[J]. Computers Fluids, 2019, 189:82-93. https://doi.org/10.1016/j.compfluid.2019.05.019

DENMAN A W, JACOBS P A, MEE D J. Compressible, turbulent flow with boundary-layer heat addition[C]//43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 2005. AIAA 2005-1097. https: //doi.org/10.2514/6.2005-1097

浏览量

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

计算气动光学研究进展

基于OpenCFD-Comb的高焓湍流边界层气体注入的直接数值模拟

高速飞行器结构/气动/推力耦合动力学建模方法

高焓流动中的可压缩颗粒求解器（第1部分）：考虑多物理效应的点力颗粒两相流理论方程

高速高温湍流研究进展