[1] |
SHU Bowen, DU Yiming, GAO Zhenghong, XIA Lu, CHEN Shusheng.
Numerical simulation of Reynolds stress model of typical aerospace separated flow
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526385-526385.
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[2] |
LIU Tingshen, FENG Lihao, WANG Jinjun.
Dynamic characteristics of hammershock in S-shaped inlet
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(2): 121339-121339.
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[3] |
WANG Hongli, XU Jinsheng, CHEN Xiong, ZHOU Changsheng.
Viscoelastic-viscoplastic constitutive model for modified double base propellant
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(4): 220505-220505.
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[4] |
XU Zhulin, DA Xingya, FAN Zhaolin.
Assessment of swirl distortion of serpentine inlet based on five-hole probe
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(12): 121342-121342.
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[5] |
CAO Yongfei, GU Yunsong, CHENG Keming, XIAO Zhongyun, CHEN Zuobin, HE Kaifeng.
Proportional control of jet deflection with passive secondary flow
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(3): 757-763.
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[6] |
AN Yuge, LIU Huoxing.
Numerical Simulation of Compressor with Inlet Distortion
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, 33(9): 1624-1632.
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[7] |
YUAN Huacheng, GUO Rongwei.
Investigation of an Experiment Project of Hypersonic Inlet with Different Forebody Widths
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2012, (4): 617-624.
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[8] |
XIE Wenzhong, GUO Rongwei.
Vortex-controlled Design Research for Serpentine Inlet
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2011, 32(10): 1806-1814.
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[9] |
Wang Zhiqiang;Hu Jun;Wang Yingfeng;Zhai Xianchao.
Aerodynamic Design of Low-speed Model Compressor for Low-speed Model Testing
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(4): 715-723.
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[10] |
Yu Xianjun;Liu Baojie;Jiang Haokang.
Three-dimensional Flows near Rotor Tip in an Axial Compressor Ⅰ—Experimental and Theoretical Studies
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(1): 48-57.
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[11] |
Yu Xianjun;Liu Baojie;Jiang Haokang.
Three-dimensional Flows near Rotor Tip in an Axial Compressor Ⅱ—Numerical Simulation Study
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2010, 31(1): 58-69.
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[12] |
Xie Lurong;Guo Rongwei.
Experimental Investigation of Fixedgeometry Two-dimensional Mixed-compression Supersonic Inlet with Twin-inlet 90° Configuration at Venter
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(6): 1000-1006.
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[13] |
Li Pu;Guo Rongwei.
Investigation of a Hypersonic Inlet with Rectangular-to-Circular Shape Transition and Forebody
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(4): 625-629.
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[14] |
Zhang Yining;Tang Hao;Wang Jiahua;Zhang Jingzhou;Han Qixiang.
Experimental Investigation on PDE Prototype with Initiator
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(3): 391-396.
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[15] |
Yan Changyu;Wu Jianjun;Liu Honggang;He Zhen.
Analysis of Impact of Laser Parameters on Performance of Lightcraft
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2009, 30(2): 193-199.
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