| Citation: | Performance of ramjet combustor based on cavity/strut structure[J]. Journal of Aerospace Power, 2017, 32(10): 2355-2363. doi: 10.13224/j.cnki.jasp.2017.10.007 |
| [1] |
ROUDAKOV A S,SCHIKHMANN Y,SEMENOV V,et al.Flight testing of an axisymmetric scramjetrussian recent acvances[R].Graz,Austria:44th Congress of the International Astronautical Federation,1993.
|
| [2] |
VINAGRADOV V,KOBIGSKY S A,PETROV M D.Experimental investigation of kerosene fuel combustion in supersonic flow[J].Journal of Propulsion and Power,1995,11(1):130-134.
|
| [3] |
LOSURDO M,BRUNO C,PATRIGNANI L.Numerical simulations of trapped vortex combustors.Feasibility study of TVC integration in traditional GT combustion chambers[R].AIAA-2006-5140,2006.
|
| [4] |
谭建国,黄国庆,潘余,等.凹腔型亚燃冲压发动机燃烧效率研究[J].航空动力学报,2011,26(6):1415-1419. TAN Jianguo,HUANG Guoping,PAN Yu,et al.Research on combustion efficiency of cavitytype ramjet[J].Journal of Aerospace Power,2011,26(6):1415-1419.(in Chinese)
|
| [5] |
SEMENOV V L,ROMANKOV O N.Operating process investigation of hydrogenfueled scramjet combustor with strut fuel feed system[R].ISABE 97-7087,1997.
|
| [6] |
HSU K Y,CARTER C D,GRUBER M R,et al.Experimental study of cavitystrut combustion in supersonic flow[J].Journal of Propulsion and Power,2010,26(6):1237-1246.
|
| [7] |
GERLINGER P,STOLL P,KINDLER M,et al.Numerical investigation of mixing and combustion enhancement in supersonic combustors by strut induced streamwise vorticity[J].Aerospace Science and Technology,2008,12(4):159-168.
|
| [8] |
FUREBY C,NORDINBATES K,PETTERSO K,et al.A computational study of supersonic combustion in strut injector and hypermixer flow fields[J].Proceedings of the Combustion Institute,2015,35(2):2127-2135.
|
| [9] |
邓远灏,钟华贵,徐华胜,等.亚燃冲压模型燃烧室高空负压试验[J].推进技术,2012,33(1):69-72.DENG Yuanhao,ZHONG Huagui,XU Huasheng,et al.Experiment of ramjet model combustor under high altitude and low pressure condition[J].Journal of Propulsion Technology,2012,33(1):69-72.(in Chinese)
|
| [10] |
谭建国,潘余,王振国.冲压发动机燃烧室内低频燃烧不稳定试验[J].推进技术,2011,32(2):188-190.TAN Jianguo,PAN Yu,WANG Zhenguo.Experimental research on lowfrequency instability in ramjet combustor[J].Journal of Propulsion Technology,2011,32(2):188-190.(in Chinese)
|
| [11] |
李庆,潘余,谭建国,等.亚燃冲压发动机中凹腔与V槽火焰稳定器性能对比分析[J].航空动力学报,2010,25(1):35-40. LI Qing,PAN Yu,TAN Jianguo,et al.Comparison of characteristics of ramjet with cavitybased flameholder and Vgutter flame holder[J].Journal of Aerospace Power,2010,25(1):35-40.(in Chinese)
|
| [12] |
李庆.基于凹腔火焰稳定器的亚燃冲压发动机燃烧室点火过程研究[D].长沙:国防科技大学,2010. LI Qing.Research on the ignition process of cavitybased flameholder in ramjet combustor[D].Changsha:National University of Defense Technology,2010.(in Chinese)
|
| [13] |
SHIH T H,LIOU W W,SHABBIR A,et al.A new kε eddy viscosity mode for high Reynolds number turbulent flow[J].Computers and Fluids,1995,24(3):227-238.
|
| [14] |
YAKHOT V,ORSSZAG S A,THANGAM S,et al.Development of turbulence models for shear flows by a double expansion technique[J].Physics of Fluids,1992,4(7):1510-1520.
|
| [15] |
MAGNUSSEN B F.On the structure of turbulence and a generalized eddy dissipation concept for chemical reaction in turbulent flow[R].AIAA -81-37570,1981.
|
| [16] |
GRAN I R,MAGNUSSEN B F.A numerical study of bluffbody stabilized diffusion flame:Part 2 influence of combustion modeling and finiterate chemistry[J].Combustion Science and Technology,1996(1/2/3/4/5/6):119-191.
|
| [17] |
POPE S B.Computationally efficient implementation of combustion chemistry using insitu adaptive tabulation[J].Combustion Theory and Modeling,1997,12(1):41-63.
|
| [18] |
ROGERS R C.Mixing of hydrogen injected from multiple injectors normal to a supersonic airstream[R].NASA TN-D-6476,1971.
|