[1] Yu Kaikai, Xu Jinglei, Tang Lan, et al. Density measurements of nozzle under over-expanded condition using background oriented schlieren technique[J]. Journal of Propulsion Technology, 2015, 36(6):832-838. (in Chinese)俞凯凯, 徐惊雷, 唐兰, 等. 基于BOS的过膨胀喷管出口密度测量[J]. 推进技术, 2015, 36(6):832-838.
[2] Wang Diankai, Hong Yanji, Li Qian, et al. Color schlieren for hypersonic shock wave structures[J]. Infrared and Laser Engineering, 2014, 43(6):1710-1714. (in Chinese)王殿恺, 洪延姬, 李倩, 等.高超声速波系结构的彩色纹影显示技术[J]. 红外与激光工程, 2014, 43(6):1710-1714.
[3] Ye Jifei,Hong Yanji. Quantitative measurement of density by color schlieren based on axial symmetry field[J]. Infrared and Laser Engineering, 2014, 43(12):3335-3338. (in Chinese)叶继飞,洪延姬. 轴对称流场的彩色纹影密度场定量测量[J]. 红外与激光工程, 2014, 43(12):3335-3338.
[4] Meng Sheng,Yang Zangjian,Wang Mingxiao. Application of quantitative schlieren method in flame temperature measurement[J]. Journal of Experiments in Fluid Mechanics, 2015, 29(4):65-69. (in Chinese)孟晟, 杨臧健, 王明晓. 纹影定量化在火焰温度测量中的应用[J]. 实验流体力学, 2015, 29(4):65-69.
[5] Lukasiewicz J. Hypersonic Experimental Method[M]. Beijing:National Defence Industrial Press, 2006:481-482.(in Chinese) J卢卡西维茨. 高超音速实验方法[M]. 国防工业出版社, 2006:481-482.
[6] Yang Zuqing. Flow Visualization Technique[M]. Beijing:National Defence Industrial Press, 2002:105-131. (in Chinese)杨祖清.流动显示技术[M]. 北京:国防工业出版社, 2002:105-131.
[7] Li Guichun. Aero-Optics[M]. Beijing:National Defence Industrial Press, 2006:411-415. (in Chinese)李桂春. 气动光学[M]. 北京:国防工业出版社, 2006:411-415.
[8] Gottlleb J. Evaluation of a double-pass schlieren system[G]. Suffield Memorandum, 1968:54-67.