Experimental Investigation of Supersonic Combustion Flame Structure with Strut Injectors
Science and Technology on Scramjet Laboratory, Institute of Aerospace and Material Engineering, National University of Defence Technology, Changsha 410073,China;Science and Technology on Scramjet Laboratory, Institute of Aerospace and Material Engineering, National University of Defence Technology, Changsha 410073,China;Science and Technology on Scramjet Laboratory, Institute of Aerospace and Material Engineering, National University of Defence Technology, Changsha 410073,China;Science and Technology on Scramjet Laboratory, Institute of Aerospace and Material Engineering, National University of Defence Technology, Changsha 410073,China
[1] Tetsuji S, Masatoshi K.Experimental Study of Strut Injectors in a Supersonic Combustor Using OH-PLIF [R].AIAA 2005-3304. [2] Chang X Y, Gu H B.Thrust and Drag of a Scramjet Model with Different Combustor Geometries [R].AIAA 2005-3315. [3] Hsu K-Y, Carter C D, Gruber M R, et al.Experimental Study of Cavity-Strut Combustion in Supersonic Flow [R].AIAA 2007-5394. [4] 范周琴.超声速湍流燃烧火焰面模型判别、建模及应用研究 [D].长沙:国防科技大学,2011. [5] 耿辉, 桑艳, 翟振辰,等.利用OH基的自发辐射图像研究凹腔在超音速燃烧中的作用 [C].三亚: 液体火箭推进技术发展研讨会, 2005. [6] 李麦亮.激光光谱诊断技术及其在火箭发动机燃烧研究中的应用 [D].长沙:国防科学技术大学, 2004. [7] 耿辉.超声速燃烧室中凹腔上游横向喷注燃料的流动、混合与燃烧特性研究 [D].长沙:国防科学技术大学, 2007. [8] 耿辉, 翟振辰, 桑艳,等.利用OH-PLIF技术显示超声速燃烧的火焰结构 [J].国防科技大学学报, 6,8 (2):1-6. [9] Micka D J, Driscoll J F.Dual-Mode Combustion of a Jet in Cross-Flow with Cavity Flameholder [R].AIAA 2008-1062. [10] 范周琴, 孙明波, 刘卫东.高温条件下火焰传播速度研究 [J].弹箭与制导学报, 1,1 (3):105-107.