1 |
张冬青, 陈英硕. 吸气式高超声速飞行器在军事领域的应用[J]. 飞航导弹, 2007(9): 14-16, 22.
|
|
ZHANG D Q, CHEN Y S. Application of air-breathing hypersonic vehicle in military field[J]. Winged Missiles Journal, 2007(9): 14-16, 22 (in Chinese).
|
2 |
刘大响, 金捷. 21世纪世界航空动力技术发展趋势与展望[J]. 中国工程科学, 2004, 6(9): 1-8.
|
|
LIU D X, JIN J. The development trends and prospect of world aeropropulsion technology in the 21st century[J]. Engineering Science, 2004, 6(9): 1-8 (in Chinese).
|
3 |
HEISER W, PRATT D, DALEY D, et al. Hypersonic airbreathing propulsion[M]. Reston: AIAA, 1994.
|
4 |
侯早, 王福民, 旷武岳. 冲压发动机超声速进气道研究进展[J]. 火箭推进, 2008, 34(5): 31-34, 58.
|
|
HOU Z, WANG F M, KUANG W Y. Development of supersonic scramjet inlet[J]. Journal of Rocket Propulsion, 2008, 34(5): 31-34, 58 (in Chinese).
|
5 |
李益文, 王宇天, 庞垒, 等. 进气道等离子体/磁流体流动控制研究进展[J]. 力学学报, 2019, 51(2): 311-321.
|
|
LI Y W, WANG Y T, PANG L, et al. Research progress of plasma/mhd flow control in inlet[J]. Chinese Journal of Theoretical and Applied Mechanics, 2019, 51(2): 311-321 (in Chinese).
|
6 |
陶淑芬. 纳秒激光脉冲烧蚀金属铜的物理过程分析[J]. 激光杂志, 2011, 32(4): 36-37.
|
|
TAO S F. The physical processes of the metallic materials in nanosecond laser ablation[J]. Laser Journal, 2011, 32(4): 36-37 (in Chinese).
|
7 |
HÄBERLE J, GÜLHAN A. Investigation of the performance of a scramjet inlet at Mach 6 with boundary layer bleed[C]∥ Proceedings of the 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference. Reston: AIAA, 2006.
|
8 |
王翼. 高超声速进气道启动问题研究[D]. 长沙: 国防科学技术大学, 2008.
|
|
WANG Y. Investigation on the starting characteristics of hypersonic inlet[D]. Changsha: National University of Defense Technology, 2008 (in Chinese).
|
9 |
OWENS L, ALLAN B, GORTON S. Boundary-layer-ingesting inlet flow control: AIAA-2006-0839[R]. Reston: AIAA,2006.
|
10 |
YAN H, GAITONDE D. Effect of thermally induced perturbation in supersonic boundary layers[J]. Physics of Fluids, 2010, 22:064101.
|
11 |
YAN H, GAITONDE D. Parametric study of pulsed thermal bumps in supersonic boundary layer[J]. Shock Waves, 2011, 21(5): 411-423.
|
12 |
FALEMPIN F, FIRSOV A A, YARANTSEV D A, et al. Plasma control of shock wave configuration in off-design mode of M=2 inlet[J]. Experiments in Fluids, 2015, 56(3): 54.
|
13 |
MENTER F R. Two-equation eddy-viscosity turbulence models for engineering applications[J]. AIAA Journal, 1994, 32(8): 1598-1605.
|
14 |
王江锋, 伍贻兆. 通风分裂算法在有限元非结构网格中的推广[J]. 中国科学技术大学学报, 1999, 29(1): 122-126.
|
|
WANG J F, WU Y Z. A new flux splitting scheme on unstructured grids: AUSM+ [J]. Journal of University of Science and Technology of China, 1999, 29(1): 122-126 (in Chinese).
|
15 |
HÄBERLE J, GÜLHAN A. Investigation of two-dimensional scramjet inlet flowfield at Mach 7[J]. Journal of Propulsion and Power, 2008, 24(3): 446-459.
|
16 |
ZHELTOVODOV A A, PIMONOV E A. Numerical simulation of an energy deposition zone in quiescent air and in a supersonic flow under the conditions of interaction with a normal shock[J]. Technical Physics, 2013, 58(2): 170-184.
|
17 |
刘凡, 严红. 脉冲能量沉积对超声速射流/激波相互作用掺混的控制研究[J]. 推进技术, 2019, 40(6): 1220-1230.
|
|
LIU F, YAN H. Mixing control of supersonic jet interacting with oblique shock by pulsed energy deposition[J]. Journal of Propulsion Technology, 2019, 40(6): 1220-1230 (in Chinese).
|
18 |
BEN-DOR G. Shock wave reflection phenomena[M]. Berlin, Heidelberg: Springer, 2007.
|
19 |
CARROLL B F, DUTTON J C. Characteristics of multiple shock wave/turbulent boundary-layer interactions in rectangular ducts[J]. Journal of Propulsion and Power, 1990, 6(2): 186-193.
|
20 |
洪延姬, 李倩, 王殿恺. 超声速飞行器的激光空气锥减阻方法[M]. 北京: 科学出版社, 2016.
|
|
HONG Y J, LI Q, WANG D K. Laser air cone drag reduction method for supersonic aircraft[M]. Beijing: Science Press, 2016 (in Chinese).
|