| [1] |
Hongyang LIU, Chao SONG, Xiao LUO, Zhu ZHOU, Guangliang LYU.
Inverse design of pressure distribution for natural laminar flow nacelle considering 3D flow effects
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(5): 126862-126862.
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| [2] |
Yongzhou LI, Di SUN, Renhua WANG, Kunyuan ZHANG.
Design of inward turning inlet with controlled Mach number under non-uniform inflow
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(12): 127857-127857.
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| [3] |
RAO Chong, ZHANG Tiejun, WEI Chuang, LIU Ying.
Influence mechanism of propeller slipstream on wing of a distributed electric aircraft scheme
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(S1): 726387-726387.
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| [4] |
CHEN Yin, GU Yunsong, SUN Zhijun, HUANG Zi.
Aerodynamic perception from distributed pressure and free flight test
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(3): 124138-124138.
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| [5] |
LI Runze, ZHANG Yufei, CHEN Haixin.
Strategies and methods for multi-objective aerodynamic optimization design for supercritical wings
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(5): 623409-623409.
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| [6] |
ZHOU Hang, JIN Zhiguang.
Micro osculating axisymmetric flow method for 3D shock wave design under nonuniform flows
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(12): 124035-124035.
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| [7] |
CAI Yiwen, JIN Zhiguang, ZHOU Jianxing, ZHOU Hang.
Design scheme of combined multiple thermodynamic cycle engine inlet
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(11): 123745-123745.
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| [8] |
HONG Junwu, WANG Yuntao, LI Wei, YANG Xiaochuan.
Numerical simulation of high-lift configuration from HiLiftPW-3
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(3): 122391-122391.
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| [9] |
LI Yiqing, HAN Weiqiang, YOU Yancheng, PAN Chengjian.
Integration waverider design of hypersonic inlet and forebody with preassigned pressure distribution
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(9): 2711-2720.
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| [10] |
LI Yongzhou, ZHANG Kunyuan, SUN Di.
Off-design performance characteristics of inward turning inlet with rectangular-to-circular shape transition with controlled Mach number distribution
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(11): 3263-3272.
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| [11] |
LI Yongzhou, ZHANG Kunyuan, SUN Di.
Experimental investigation on a hypersonic inward turning inlet of rectangular-to-circular shape with controlled Mach number distribution
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016, 37(10): 2970-2979.
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| [12] |
LI Yongzhou, ZHANG Kunyuan.
Integrated design of forebody and inlet based on external and internal conical basic flow field with controlled Mach number distribution surface
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(1): 289-301.
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| [13] |
GUO Shanguang, WANG Zhenguo, ZHAO Yuxin, FAN Xiaoqiang.
Inverse Design of the Fore-body Curved Shock Wave of the Hypersonic Planar Inlet
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(5): 1246-1256.
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| [14] |
SONG Yanming, YANG Yang.
Numerical Simulation of Hydrostatic Bearing with Self-controlled Restrictor Employing Cooling Roll in Amorphous Alloy Ribbon Formation
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(4): 1157-1164.
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| [15] |
YANG Kunmiao, ZHANG Weimin, WANG Bin.
Research of Supercritical Wing Optimization Based on Aerodynamic Design Principle of Wing
[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2013, 34(2): 263-272.
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