Numerical simulation of dual shear coaxial gas-gas injector

[1] Calhoon D, Ito J, Kors D. Investigation of gaseous propellant combustion and associated injector chamber design guidelines .NASA CR-121234,1973 [2] Foust M, pal S, Santoro R.Gaseous propellant rocket studies using raman spectorscopy . AlAA-1996-2766, 1996 [3] Jones A,Groot W. Oxygen temperature and concentration measurements in H₂-O₂ rocket engines . AIAA-1996-0439, 1996  [4] Foust M, Deshpande M, Pal S.Experimental and analytical characterization of a shear coaxial combusting GO2/G2 flowfield . AlAA-1996-0646, 1996 [5] Jacques B, Martin S. Tricoaxial injector technology development . AlAA-1999-2492,1999 [6] Fournet A,Lonchard J,Thomas J. Technological demonstration for low cost gas generator . AIAA-2004-4006, 2004 [7] 程圣清,宋连忠,王珏.氢氧火箭发动机预燃室喷注器特性研究[J].导弹与航天运载技术,1998,5(1):6-15 Cheng Shengqing,Song Lianzhong,Wang Jue.The study of preburner injector character istics for the hydrogen-oxygen engine[J].Missiles and Space Vehicles, 1998, 5(1):6-15(in Chinese) [8] 中国航天工业总公司.世界导弹与航天发动机大全[M].北京:军事科学出版社, 1999:116 China Aerospace Science and Industry Corporation. An encyclopedia of world missile and space engine[M]. Beijing: Military Science Press, 1999:116(in Chinese) [9] Shang M, Chen Y, Paul L. Investigation of chemical kenetics integration algorithms for reacting flows . AIAA-1995-0806, 1995