[1] 殷兴良. 气动光学原理[M]. 北京:中国宇航出版社, 2003. [2] 殷兴良. 现代光学新分支学科-气动光学[J]. 中国工程科学, 2005,7(12):1-2. [3] 殷兴良.高速飞行器气动光学传输效应的工程计算方法[J].中国工程科学, 2006, 8(11):74-79. [4] 史可天, 马汉东. 可压缩混合层气动光学效应研究[J].计算物理, 2010, 27(1):65-72. [5] 费锦东.气动光学效应校正技术初步分析[J]. 红外与激光工程.1999,28(5):10-17. [6] 张丽琴,费锦东.气动光学效应光电校正方法研究[J].红外与激光工程, 2004, 33(6):580-583. [7] 陈澄,费锦东.侧窗头罩高速层流流场光学传输效应数值模拟[J]. 红外与激光工程,2005,34(5):548~552. [8] CLARK R L, FARRIS R C. A numerical method to predict aero-optical performance in hypersonic flight[J]. AIAA, 1987:1396. [9] GIERLOFF J J, ROBERTSON S J, BOUSKA D H. Computer analysis of aero-optic effects[J].AIAA, 1992:2794. [10] CHANG K, LI C. Evaluation of mixing length in a planar mixing layer based on shear-induced vortex quantity[J]. AIAA, 2009:4172. [11] MOHAMMED KAMEL, KAN WANGY, MENG WANG. Predictions of aero-optical distortions using LES with wall modeling[J]. AIAA, 2016:1462. [12] GRINSTEIN F F, FUREBY C. Recent progress on MILES for high Reynolds number flows[J]. Journal of Fluids Engineering, 2002, 124(4):848-861. [13] 傅德薰,马延文.可压混合层流动转捩到湍流的直接数值模拟[J]. 中国科学, 2000, A30(2):162-168. [14] 马汉东, 潘宏禄, 王强. 超声速平板边界层斜波失稳转捩过程研究[J]. 力学学报, 2007, 39(2):153-157. [15] WU M, BOOKEY P, MARTINS M P, et al. Analysis of shockwave/turbulent boundary layer interaction using MILES and experimental data[J]. AIAA, 2005:310. [16] HORSTMAN C C, SETTLES G S, et al. A reattaching free shear layer in compressible turbulent flow:A comparison of numerical and experimental results[J]. AIAA,1981:0333. |