Recent research progress on flame characteristics in strut-equipped scramjet combustor

ZHANG Junlong; CHANG Juntao; WANG Xuan; BAO Wen

doi:10.7638/kqdlxxb-2019.0168

English Version Journal Login

您当前的位置：

首页 >

文章列表页 >

Recent research progress on flame characteristics in strut-equipped scramjet combustor

更新时间：2026-05-28

- Recent research progress on flame characteristics in strut-equipped scramjet combustor
- Vol. 38, Issue 3, Pages: 577-592(2020)
- 作者机构：
  
  哈尔滨工业大学能源科学与工程学院,哈尔滨,150001
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2019.0168
  CLC： V434+.13;TQ038
- Published：2020
- 稿件说明：
移动端阅览
张军龙, 常军涛, 王瑄, 鲍文. 基于支板稳燃的超声速火焰特性研究进展[J]. 空气动力学学报, 2020, 38(3): 577-592.

ZHANG Junlong, CHANG Juntao, WANG Xuan, et al. Recent research progress on flame characteristics in strut-equipped scramjet combustor[J]. 2020, 38(3): 577-592.
张军龙, 常军涛, 王瑄, 鲍文. 基于支板稳燃的超声速火焰特性研究进展[J]. 空气动力学学报, 2020, 38(3): 577-592. DOI： 10.7638/kqdlxxb-2019.0168.

ZHANG Junlong, CHANG Juntao, WANG Xuan, et al. Recent research progress on flame characteristics in strut-equipped scramjet combustor[J]. 2020, 38(3): 577-592. DOI： 10.7638/kqdlxxb-2019.0168.

摘要

以超燃冲压发动机燃烧室为主要研究对象，对超声速气流中的火焰稳定机理及火焰传播特性的研究进展进行了综述，涵盖了不同稳燃器的超声速燃烧室中的火焰特性及火焰稳燃机理分析、火焰传播及振荡特性等研究内容，旨在揭示超声速气流中的火焰特征并进一步实现燃烧室的性能优化，以期对超声速燃烧室的火焰特性相关研究提供一定的参考。首先，从燃烧室流动及燃料驻留时间的角度分析了超声速火焰稳定的难点，进一步分析了超声速燃烧室中火焰稳定的基本判据，总结了当前两种主流的火焰稳燃模式，分析了支板稳燃器在增强燃料掺混方面的优势，并以支板稳燃为主要侧重点进行了后续火焰特性的研究；其次，从增加燃料驻留时间和减小燃料化学反应时间两个角度总结了当前实现超声速火焰稳定的基本方法及稳燃原理。最后，讨论了火焰稳定之后的燃烧室火焰动态特性，包括火焰传播特性和火焰振荡特性，为后续的燃烧优化提供参考。

Abstract

Scramjets are regarded as one of the most efficiency air-breathing propulsion devices in supersonic flight conditions

and combustors are critical components in scramjet engines. In supersonic combustor

the velocity of the main airflow is of an order of kilometers per second

and in such a harsh flowing condition

the combustion organization and flame stabilization are extremely hard to be achieved. To solve the issues about flame holding and combustion efficiency improving

it is necessary to have a deep understanding in the flame characteristics

based on which

the further optimization could be carried out. In superson

ic combustor

the flame characteristics including the flame mechanism characteristic and the flame propagation characteristic should be paid more attention. This paper aims to provide a review on flame stabilization and flame propagation characteristics in supersonic combustor to help the researchers easily working on supersonic combustion with their further work. At first

the difficulty on the flame stabilization is discussed

including the higher airflow velocity and lower fuel resident time in the combustor. Furthermore

the flame characteristic in supersonic combustor in two kinds of main flame stabilization modes

namely the cavity and the strut

are summarized

and the advantage of strut in fuel injection and fuel mixing performance is set forth. The flame stabilization criteria are also presented and analyzed. Then

the methods of flame stabilization

including enlarging the fuel resident time and shortening the fuel reaction time

are also reported

and the mechanism of flame stabilization in different flame holding schemes are analyzed. The O

-pilot strut designed by Harbin Institute of Technology is focused on

and the dynamic characteristics

including flame propagation and flame oscillation characteristics

are analyzed. The flame propagation characteristic in strut/wall combined fuel injection mode is discussed. Based on this paper

the improved scheme of combustion performance is given to provide a reference for the further investigation.

关键词

Keywords

references

CHANG J T, ZHANG J L, BAO W, et al. Research progress on strut-equipped supersonic combustors for scramjet application[J]. Progress in Aerospace Sciences, 2018, 103:1-30. https://doi.org/10.1016/j.paerosci.2018.10.002

WANG J F, WANG X D, LI J W, et al. Overview on aerodynamic design of cruising waverider configuration for hypersonic vehicles[J]. Acta Aerodynamica Sinica, 2018, 36(5):705-728. (in Chinese)

CURRAN E T. Scramjet engines:the first forty years[J]. Journal of Propulsion and Power, 2001, 17(6):1138-1148. https://doi.org/10.2514/2.5875

ZHANG J L. Combustion characteristics in supersonic combustor equipped with strut/wall fuel injection[D]. Harbin: Harbin Institute of Technology, 2015. (in Chinese)

QIN J, ZHANG S L, BAO W, et al. Thermal management method of fuel in advanced aeroengines[J]. Energy, 2013, 49:459-468. https://doi.org/10.1016/j.energy.2012.10.050

ZHANG S L, QIN J, BAO W, et al. Thermal management of fuel in advanced aeroengine in view of chemical recuperation[J]. Energy, 2014, 77:201-211. https://doi.org/10.1016/j.energy.2014.06.071

宁东坡.超声速燃烧室长时间工作稳燃支板性能研究[D].哈尔滨: 哈尔滨工业大学, 2015.

WANG Z G, WANG H B, SUN M B. Review of cavity-stabilized combustion for scramjet applications[J]. Proceedings of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2014, 228(14):2718-2735. https://doi.org/10.1177/0954410014521172

ZHAO D, GUTMARK E, de GOEY P. A review of cavity-based trapped vortex, ultra-compact, high-g, inter-turbine combustors[J]. Progress in Energy and Combustion Science, 2018, 66:42-82. https://doi.org/10.1016/j.pecs.2017.12.001

MAI T, SAKIMITSU Y, NAKAMURA H, et al. Effect of the incident shock wave interacting with transversal jet flow on the mixing and combustion[J]. Proceedings of the Combustion Institute, 2011, 33(2):2335-2342. https://doi.org/10.1016/j.proci.2010.07.056

HU J C. Ignition and flame stabilization in a flush wall supersonic combustor[D]. Harbin: Harbin Institute of Technology, 2014. (in Chinese)

ZHU L, LUO F, QI Y Y, et al. Effects of spray angle variation on mixing in a cold supersonic combustor with kerosene fuel[J]. Acta Astronautica, 2018, 144:1-11. https://doi.org/10.1016/j.actaastro.2017.12.013

SCHETZ J A, BILLIG F S. Penetration of gaseous jets injected into a supersonic stream[J]. Journal of Spacecraft and Rockets, 1966, 3(11):1658-1665. https://doi.org/10.2514/3.28721

FULLER E J, MAYS R B, THOMAS R H, et al. Mixing studies of helium in air at high supersonic speeds[J]. AIAA Journal, 1992, 30(9):2234-2243. https://doi.org/10.2514/3.11210

LEE S H, SHIN H B, MITANI T. Mixing and combustion augmentations of transverse injection in scramjet combustor[ C ] //39th Aerospace Sciences Meeting and Exhibit, Reno, NV, USA. Reston, Virigina: AIAA, 2001. https://doi.org/10.2514/6.2001-384

VINOGRADOV V A, SHIKHMAN Y M, ALBEGOV R V, et al. About possibility of effective methane combustion in high speed subsonic airflow[R]. AIAA 2002-5206, 2002.

VINOGRADOV V, SHIKHMAN Y, ALBEGOV R, et al. Experimental research of pre-injected methane combustion in high-speed subsonic airflow[C ] //12th AIAA International Space Planes and Hypersonic Systems and Technologies. Norfolk, Virginia. Reston, Virigina: AIAA. AIAA 2003-6940. https://doi.org/10.2514/6.2003-6940

YU G, LI J G, CHEN L H, et al. Investigation on selfignition characteristics of kerosene hydrogen dual fuel in supersonic Combustor[J]. Experiments and Measurements in Fluid Mechanics, 2000, 14(1):63-71. (in Chinese)

BOGDANOFF D W. Advanced injection and mixing techniques for scramjet combustors[J]. Journal of Propulsion and Power, 1994, 10(2):183-190. https://doi.org/10.2514/3.23728

CANDON M J, OGAWA H. Numerical analysis and design optimization of supersonic after-burning with strut fuel injectors for scramjet engines[J]. Acta Astronautica, 2018, 147:281-296. https://doi.org/10.1016/j.actaastro.2018.04.012

VISHWAKARMA M, VAIDYANATHAN A. Experimental study of mixing enhancement using pylon in supersonic flow[J]. Acta Astronautica, 2016, 118:21-32. https://doi.org/10.1016/j.actaastro.2015.09.011

HSU K Y, CARTER C D, GRUBER M R, et al. Mixing study of strut injectors in supersonic flows[C ] //45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit. Denver, Colorado, 2009. AIAA 2009-5226. https://doi.org/10.2514/6.2009-5226

Bagg C, Greendyke R. Computational analysis of strut induced mixing in a scramjet[C ] //47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition. Orlando, Florida, 2009. AIAA 2009-1253. https://doi.org/10.2514/6.2009-1253

TAM C J, HSU K Y, GRUBER M, et al. Fuel/air mixing characteristics of strut injections for scramjet combustor applications[C ] //26th AIAA Applied Aerodynamics Conference, Honolulu, Hawaii. Reston, Virigina: AIAA. AIAA 2008-6925. https://doi.org/10.2514/6.2008-6925

Tam C J, Hsu K Y, Gruber M, et al. Aerodynamic Performance of Strut Injection for a Round Scramjet Combustor[C ] //43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit. Cincinnati, OH. AIAA 2007-5403. https://doi.org/10.2514/6.2007-5403

CHOUBEY G, PANDEY K M. Effect of parametric variation of strut layout and position on the performance of a typical two-strut based scramjet combustor[J]. International Journal of Hydrogen Energy, 2017, 42(15):10485-10500. https://doi.org/10.1016/j.ijhydene.2017.03.014

CHOUBEY G, PANDEY K M. Effect of different strut + wall injection techniques on the performance of two-strut scramjet combustor[J]. International Journal of Hydrogen Energy, 2017, 42(18):13259-13275. https://doi.org/10.1016/j.ijhydene.2017.04.024

MANNA P, BEHERA R, CHAKRABORTY D. Liquid-fueled strut-based scramjet combustor design:a computational fluid dynamics approach[J]. Journal of Propulsion and Power, 2008, 24(2):274-281. https://doi.org/10.2514/1.28333

KUMARAN K, BEHERA P R, BABU V. Numerical investigation of the supersonic combustion of kerosene in a strut-based combustor[J]. Journal of Propulsion and Power, 2010, 26(5):1084-1091. https://doi.org/10.2514/1.46965

DESIKAN S L N, KURIAN J. Strut-based gaseous injection into a supersonic stream[J]. Journal of Propulsion and Power, 2006, 22(2):474-477. https://doi.org/10.2514/1.16770

MITANI T, CHINZEI N, KANDA T. Reaction and mixing-controlled combustion in scramjet engines[J]. Journal of Propulsion and Power, 2001, 17(2):308-314. https://doi.org/10.2514/2.5743

M. HANK J, S. MURPHY J, MUTZMAN R C. The X-51A Scramjet Engine flight demonstration program[C ] //15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. Dayton, Ohio. AIAA 2008-2540. https://doi.org/10.2514/6.2008-2540

LE J L, YANG S H, LI H B. Analysis and correlation of flame stability limits in supersonic flow with cavity flameholder[C ] //18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France. Reston, Virigina: AIAA. AIAA 2012-5948. https://doi.org/10.2514/6.2012-5948

SATHIYAMOORTHY K, DANISH T H, SRINIVAS J, et al. Experimental investigation of supersonic combustion in a strut-cavity based combustor[J]. Acta Astronautica, 2018, 148:285-293. https://doi.org/10.1016/j.actaastro.2018.05.014

BEN-YAKAR A, HANSON R K. Cavity flame-holders for ignition and flame stabilization in scramjets:an overview[J]. Journal of Propulsion and Power, 2001, 17(4):869-877. https://doi.org/10.2514/2.5818

BAO W, ZONG Y H, CHANG J T, et al. Effects of upstream strut on the combustion of liquid kerosene in a model cavity scramjet[J]. Proceedings of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2014, 228(12):2323-2328. https://doi.org/10.1177/0954410013515370

ZONG Y H, BAO W, CHANG J T, et al. Effect of fuel injection allocation on the combustion characteristics of a cavity-strut model scramjet[J]. Journal of Aerospace Engineering, 2015, 28(1):04014050. https://doi.org/10.1061/(asce)as.1943-5525.0000374

GHODKE C, CHOI J, SRINIVASAN S, et al. Large eddy simulation of supersonic combustion in a cavity-strut flameholder[C ] //49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, Florida. Reston, Virigina: AIAA. AIAA 2011-323. https://doi.org/10.2514/6.2011-323

Chang X Y, Gu H B, Chen L H. Thrust and drag of a scramjet model with different combustor geometries[C ] //AIAA/CIRA 13th International Space Planes and Hypersonics Syst ems and Technologies Conference. Capua, Italy. AIAA 2005-3315. https://doi.org/10.2514/6.2005-3315

CHEN L H, GU H B, ZHANG X Y. Experimental study on scram jet with cavity/strut configuration[J]. Journal of Engineering Thermophysics, 2007, 28(4):717-719. (in Chinese)

ZHU S H, XU. Experimental study on flame transition in a two-stage struts dual-mode scramjet[J]. Journal of Aerospace Engineering, 2017, 30(5):06017002. https://doi.org/10.1061/(asce)as.1943-5525.0000740

ZHU S H, XU, JI P F. Flame stabilization and propagation in dual-mode scramjet with staged-strut injectors[J]. AIAA Journal, 2017, 55(1):171-179. https://doi.org/10.2514/1.j054974

ZHU S H, XU, YANG Q C, et al. Intermittent back-flash phenomenon of supersonic combustion in the staged-strut scramjet engine[J]. Aerospace Science and Technology, 2018, 79:70-74. https://doi.org/10.1016/j.ast.2018.05.037

YANG Q C, CHETEHOUNA K, GASCOIN N, et al. Experimental study on combustion modes and thrust performance of a staged-combustor of the scramjet with dual-strut[J]. Acta Astronautica, 2016, 122:28-34. https://doi.org/10.1016/j.actaastro.2016.01.002

YANG Q C, BAO W, ZONG Y H, et al. Combustion characteristics of a dual-mode scramjet injecting liquid kerosene by multiple struts[J]. Proceedings of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2015, 229(6):983-992. https://doi.org/10.1177/0954410014542447

Vinogradov V, Shikhman Y, Albegov R, et al. Experimental Research of Pre-Injected Methane Combustion in High-Speed Subsonic Airflow[C ] //12th AIAA International Space Planes and Hypersonic Systems and Technologies. Norfolk, Virginia. AIAA 2003-6940. https://doi.org/10.2514/6.2003-6940

WANG L, WU Y C, LE J L. Numerical simulations of hydrogen-fueled scramjet combustor flowfields on unstructured grid[J]. Acta Aerodynamica Sinica, 2009, 27(3):308-313. (in Chinese)

OEVERMANN M. Numerical investigation of turbulent hydrogen combustion in a SCRAMJET using flamelet modeling[J]. Aerospace Science and Technology, 2000, 4(7):463-480. https://doi.org/10.1016/s1270-9638(00)01070-1

Fuhrmann S, Hupfer A, Kau H P. Investigations on Multi-Stage Supersonic Combustion in a Model Combustor[C ] //17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. San Francisco, Calif ornia.AIAA 2011-2332. https://doi.org/10.2514/6.2011-2332

BERGLUND M, FEDINA E, FUREBY C, et al. Finite rate chemistry large-eddy simulation of self-ignition in supersonic combustion ramjet[J]. AIAA Journal, 2010, 48(3):540-550. https://doi.org/10.2514/1.43746

YU G, LI J G, CHANG X Y, et al. Investigation of kerosene combustion characteristics with pilot hydrogen in model supersonic combustors[J]. Journal of Propulsion and Power, 2001, 17(6):1263-1272. https://doi.org/10.2514/2.5874

LEONOV S B, YARANTSEV D A. Plasma-induced ignition and plasma-assisted combustion in high-speed flow[J]. Plasma Sources Science and Technology, 2007, 16(1):132-138. https://doi.org/10.1088/0963-0252/16/1/018

DO H, IM S K, CAPPELLI M A, et al. Plasma assisted flame ignition of supersonic flows over a flat wall[J]. Combustion and Flame, 2010, 157(12):2298-2305. https://doi.org/10.1016/j.combustflame.2010.07.006

BAO W, HU J C, ZONG Y H, et al. Combustion characteristic using O 2 -pilot strut in a liquid-kerosene-fueled strut-based dual-mode scramjet[J ] . Proceedings of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2013, 227(1 2):1870-1880. https://doi.org/10.1177/0954410012464455

HU J C, QIN J, CHANG J T, et al. Combustion stabilization based on a center flame strut in a liquid kerosene fueled supersonic combustor[J]. Journal of Thermal Science, 2013, 22(5):497-504. https://doi.org/10.1007/s11630-013-0654-6

ZHANG J L, CHANG J T, MA J C, et al. Local and global flame characteristics in a liquid kerosene fueled supersonic combustor equipped with a thin strut[J]. Aerospace Science and Technology, 2018, 76:49-57. https://doi.org/10.1016/j.ast.2018.02.007

ZHANG J L, CHANG J T, MA J C, et al. Investigation of flame establishment and stabilization mechanism in a kerosene fueled supersonic combustor equipped with a thin strut[J]. Aerospace Science and Technology, 2017, 70:152-160. https://doi.org/10.1016/j.ast.2017.08.005

SUMMERFIELD M. Injection and mixing in turbulent flow[M]. New York:American Institute of Aeronautics and Astronautics, Inc., 1980. https://doi.org/10.2514/4.865428

MITANI T, KOUCHI T. Flame structures and combustion efficiency computed for a Mach 6 scramjet engine[J]. Combustion and Flame, 2005, 142(3):187-196. https://doi.org/10.1016/j.combustflame.2004.10.004

RASMUSSEN C C, DHANUKA S K, DRISCOLL J F. Visualization of flameholding mechanisms in a supersonic combustor using PLIF[J]. Proceedings of the Combustion Institute, 2007, 31(2):2505-2512. https://doi.org/10.1016/j.proci.2006.08.007

袁生学.论超声速燃烧[J].中国科学(A辑), 1998, 28(8):735-741.https://doi.org/10.1360/za1998-28-8-735

FAN Z Q, LIU W D, SUN M B. The research on flame speed at high temperature[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2011, 31(3):105-107. (in Chinese)

SUN M B, CUI X D, WANG H B, et al. Flame flashback in a supersonic combustor fueled by ethylene with cavity flameholder[J]. Journal of Propulsion and Power, 2015, 31(3):976-981. https://doi.org/10.2514/1.b35580

HU J C, BAO W, CHANG J T. Flame transition in dual-mode scramjet combustor with oxygen piloted ignition[J]. Journal of Propulsion and Power, 2014, 30(4):1103-1107. https://doi.org/10.2514/1.b35239

ZHANG J L, CHANG J T, WANG Z A, et al. Flame propagation and flashback characteristics in a kerosene fueled supersonic combustor equipped with strut/wall combined fuel injectors[J]. Aerospace Science and Technology, 2019, 93:105303. https://doi.org/10.1016/j.ast.2019.105303

XIAO B G, XING J W, TIAN Y, et al. Experimental and numerical investigations of combustion mode transition in a direct-connect scramjet combustor[J]. Aerospace Science and Technology, 2015, 46:331-338. https://doi.org/10.1016/j.ast.2015.08.001

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

BAO W, YANG Q C, CHANG J T, et al. Dynamic characteristics of combustion mode transitions in a strut-based scramjet combustor model[J]. Journal of Propulsion and Power, 2013, 29(5):1244-1248. https://doi.org/10.2514/1.b34921

ZHANG C L, CHANG J T, FENG S, et al. Pressure rising slope variation accompanying with combustion mode transition in a dual-mode combustor[J]. Aerospace Science and Technology, 2017, 68:370-379. https://doi.org/10.1016/j.ast.2017.05.034

ZHANG C L, CHANG J T, ZHANG Y S, et al. Flow field characteristics analysis and combustion modes classification for a strut/cavity dual-mode combustor[J]. Acta Astronautica, 2017, 137:44-51. https://doi.org/10.1016/j.actaastro.2017.03.023

ZHANG C L, CHANG J T, MA J X, et al. Effect of Mach number and equivalence ratio on the pressure rising variation during combustion mode transition in a dual-mode combustor[J]. Aerospace Science and Technology, 2018, 72:516-524. https://doi.org/10.1016/j.ast.2017.11.042

HU J C, CHANG J T, BAO W, et al. Experimental study of a flush wall scramjet combustor equipped with strut/wall fuel injection[J]. Acta Astronautica, 2014, 104(1):84-90. https://doi.org/10.1016/j.actaastro.2014.07.012

ZHANG J L, CHANG J T, TIAN H M, et al. Flame interaction characteristics in scramjet combustor equipped with strut/wall combined fuel injectors[J]. Combustion Science and Technology, 2019:1-24. https://doi.org/10.1080/00102202.2019.1627342

HUANG Z W, HE G Q, QIN F, et al. Combustion oscillation study in a kerosene fueled rocket-based combined-cycle engine combustor[J]. Acta Astronautica, 2016, 129:260-270. https://doi.org/10.1016/j.actaastro.2016.09.024

HUANG Z W, HE G Q, WANG S, et al. Simulations of combustion oscillation and flame dynamics in a strut-based supersonic combustor[J]. International Journal of Hydrogen Energy, 2017, 42(12):8278-8287. https://doi.org/10.1016/j.ijhydene.2016.12.142

WANG H B, WANG Z G, SUN M B. Experimental study of oscillations in a scramjet combustor with cavity flameholders[J]. Experimental Thermal and Fluid Science, 2013, 45:259-263. https://doi.org/10.1016/j.expthermflusci.2012.10.013

WANG H B, WANG Z G, SUN M B, et al. Large-Eddy/Reynolds-averaged Navier-Stokes simulation of combustion oscillations in a cavity-based supersonic combustor[J]. International Journal of Hydrogen Energy, 2013, 38(14):5918-5927. https://doi.org/10.1016/j.ijhydene.2013.02.100

WANG Z G, SUN M B, WANG H B, et al. Mixing-related low frequency oscillation of combustion in an ethylene-fueled supersonic combustor[J]. Proceedings of the Combustion Institute, 2015, 35(2):2137-2144. https://doi.org/10.1016/j.proci.2014.09.005

OUYANG H, LIU W D, SUN M B. Parametric study of combustion oscillation in a single-side expansion scramjet combustor[J]. Acta Astronautica, 2016, 127:603-613. https://doi.org/10.1016/j.actaastro.2016.05.002

ZHANG J L, CHANG J T, KONG C, et al. Flame oscillation characteristics in a kerosene fueled dual mode combustor equipped with thin strut flameholder[J]. Acta Astronautica, 2019, 161:222-233. https://doi.org/10.1016/j.actaastro.2019.05.037

Views

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Hydrogen combustion experiments of a fullpath scramjet at a Mach 10 condition of high enthalpy shock tunnel

Thrust/Drag measurement techniques of a free flight scramjet in a shock tunnel

Modeling methodology for complex chemical mechanism involved in supersonic combustion simulation

Overview on the research progress of unsteady supersonic combustion

Progress of the studies on the extension of flamelet models to supersonic combustion flows

Related Author

WEI Baoxi

YANG Fujiang

ZHU Hao

WANG Ruiting

LIU Chunfeng

WU Hengyi

JI Feng

CHEN Xing

Related Institution

China Academy of Aerospace Aerodynamics, Beijing

Engineering and Materials Science Center, University of Science and Technology of China, Hefei

Beijing Power Machinery Institute, Beijing

State Key Laboratory of High Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences

School of Engineering Science, University of Chinese Academy of Sciences

AI问答

⁰