[1] Aguilera C, Pang B,Yu K H.Fin-Guided Liquid-Feul injection ito March 2.1 Airflow[R].AIAA 2011-5763. [2] Chae-Hyoung Kim,In-Seuck Jeung.Effect of Fuel Injection Locations with Hyper Mixer in Supersonic Combustion[R].AIAA 2011-5830. [3] Jan Martinze Schranmm, Sebastian Karl,Klaus Hnnemann.Ground Testing of the HyShot II Scramjet Configuration in HEG[R].AIAA 2008-2547. [4] Fan Xuejun,Yu Gong,Li Jianguo, et al.Investigation of Vaporized Kerosene Injection and Combustion in a Supersonic Model Combustion[J].Journal of Propulsion and Power, 6,2(1). [5] Lavante E Von,Zeitz D,Kallenberg M.Numerical Simulation of Supersonic Airflow with Transverse Hydrogen Injection[J].Journal of Propulsion and Power,1,7(6). [6] Kondo A, Sakaue S, Arai T.Fluctuation of Mass Flux and Concentration on Supersonic Mixing using Streamwise Vortices[R].AIAA 2008-2535. [7] Chae Hyoung Kim, Eunju Jeong, Jeong-Woo Kim, et al.Mixing and Penetration Studies of Transverse Jet into a Supersonic Crossflow[R].AIAA 2007-5420. [8] Bonanos Aristides M, Bergthorson Jeffrey M,Dimotakis Paul E.Molecular Mixing and Flowfield Measurements in an Expansion-Ramp Combustion:Supersonic Flow[R].AIAA 2007-5417. [9] Tomoaki KitagawaIgnition, Atsushi Moriwaki, Kenichi Takita, et al.Characteristics of Methane and Hydrogen Using a Plasma Torch in Supersonic Flow[J].Journal of Propulsion and Power, 3,9(5). [10] Koichi Murakami, Aya Nishikawa, Kenichi Takita, et al.Ignition Characteristics of Hydrocarbon Fuels by Plasma Torch in Supersonic Flow[R].AIAA 2003-6939. [11] Jinkwan Song, Chanyeon Jung, Jeongjae Hwang, et al.An Experimental Study on the Flame Dynamics with V-Gutter Typer Flameholder in the Model Combustor[R].AIAA 2011-6126. [12] Sergey Leonov,Dmitry Yaeantsev.Eeperiments on Electrically Controlled Flameholding on a Plane Wall in Supersonic Airflow[J].Journal of Propulsion and Power,9,5(2). [13] Rasmussen Chadwick C,Driscoll James F.Characteristics of Cavity-Stabilized Flames in a Supersonic Flow[J].Journal of Propulsion and Power,5,1(4). [14] Estruch D, Lawson N J,MacManus D G, et al.Measurement of Shock Wave Unsteadiness using a High-Speed Schlieren System and Digital Image Processing[J].Review of Scentific Instruments,2008,9,8. [15] Sugiyama H,Tsujiguchi Y,Honma T.Structure and Oscillation Phenomena of Pseudo-Shock Wave in a Straight Square Duct at Mach2 and 4[R].AIAA 2008-2646. [16] Tsuyoshi Kumasaka, Noritaka Ichikawa, Goro Masuya, et al.Influence of Combustion on Behavior of Pesudo-Shock Wave[R].AIAA 2003-6912. [17] Ferry F J Schrijer, Fulvio Scarano,Bas W van Oudheusden.Experiments on Hypersonic Boundary Layer Separation and Reattachment on a Blunted Cone-Flare using Quantitative InfraRed Thermography[R].AIAA 2003-6967. [18] Pan Yu, Tan Jian-Guo,Liang Jian-Han, et al.Experimental Investigation of Combustion Mechanisms of Kerosene-Fueled Scramjet Engines with Double-Cavity Flameholders[J].Acta Mechanica Sinica, 1,7(6). [19] Pan Yu, Lei Jing, Tan Jianguo, et al.Experimental Investigation on the Combustion Oscillation in a Model Scramjet Engine[R].ISABE 2011-1528. [20] Liepmann H W.Elements of Gasdynamics[M].New York:John Wiley & Sons.Inc, 1957. [21] Fan X J, Zhong F Q, Yu G,et al.Catalytic Cracking and Heat Sink Capacity of Aviation Kerosene under Supercritical Conditions[J].Journal of Propulsion and Power,9,5(6). [22] 范学军, 俞刚.超临界煤油超声速燃烧特性实验[J].推进技术, 6,7 (1).(FAN Xue-jun,YU Gang.Experiments on Supersonic Combustion of Supercritical Kerosene[J].Journal of Propulsion Technology,6,7(1).)
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