HSU K Y L P G, TRUMP D D, ROQUEMORE W M. Performance of a trapped？vortex combustor, AIAA 95？0810[R]. Reno，NV: 33rd Aerospace Sciences Meeting and Exhibit,1995.？
？GAN Zhiwen. Study on the transient flow field in the trapped vortex combustor [D].Beijing: Beijing University of Aeronautics and Astronautics, 2003: 3？
[4]
XING Fei, WANG Peiyong. Experimental investigation of a single trapped？vortex combustor with a slight temperature raise[J]. Aerospace Science and Technology, 2010:1？6.
？WANG Xiaodong, LE Jialing, SONG Wenyan. Study to the combustion performance of a scramjet combustor with struts[J]. Acta Aerodynamica Sinica, 2004. 22(3): 274？278.？
[7]
周校平，张晓男, 燃烧理论基础[M].上海: 上海交通大学出版社出版,2001:91？93.
[8]
VISWANATH R,KATTA W M R.Study on trapped？vortex combustor effect of injection on dynamics of non？reacting and reacting flows in a cavity[J].Journal of Propulsion and Power,1997,14(3):273？281.
[9]
VISWANATH R, KATTA W M R.Simulation of unsteady flows in an axisymmetric research combustor using detailed？chemical kinetics[R].Cleveland, OH: 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit,1998.？
[10]
DONALD K B, SHAWN P. Trapped vortex combustor: United States,US 2004/0020211 A1[P].2004？01？29.？
HE Xiaomin, WANG Jiahua. An investigation on the fluid characteristics of trapped？vortex combustor[J].Journal of Aerospace Power,2002,7(5): 567？571.
[14]
XING Fei, ZHANG Rongchun, FAN Weijun,et al. Experiment study on single/ fuel？lean trapped vortex combustor ignition and limit blow？out at different main air and mix air temperatures[J].Journal of Aerospace Power,2008,23(12):2280？2285.
[15]
丁阳.驻涡燃烧室燃烧特性的数值模拟[D].沈阳:沈阳航空工业学院, 2009: 4？6.
[16]
？DING Yang. Numerical simulation of comcustion performances of the trapped vortex comcustor [D]. Shenyang: Shenyang Institute of Aeronautical Engineering, 2009:4？6.？
[17]
HSU K Y, KATTA V R.Characteristics of combustion instability associated with trapped vortex burner, AIAA 99？0488[R]. Reno, NV: 37th AIAA Aerospace Sciences Meeting and Exhibit,1999.？
[18]
HENDRICKS R C, ROQUEMORE W M,et al.Experimental and Computational study of trapped vortex combustor sector rig with tri？pass diffuser, NASA/TM？2004？212507 [R].Hanover, MD: National Aeronautics and Space Administration Glenn Research Center,2004.
