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Acta Aeronautica et Astronautica Sinica: 50 years of development
CAI Fei, GE Jianping
doi: 10.7527/S1000-6893.2015.0255
2015, (8): 2497-2506.
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Study of supersonic commercial transport and reduction of sonic boom
ZHU Ziqiang, LAN Shilong
doi: 10.7527/S1000-6893.2014.0207
2015, (8): 2507-2528.
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Research progresses of stall precursor-suppressed casing treatment
SUN Xiaofeng, SUN Dakun
doi: 10.7527/S1000-6893.2015.0153
2015, (8): 2529-2543.
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Precooling technology study of hypersonic aeroengine
ZOU Zhengping, LIU Huoxing, TANG Hailong, WAN Min, WANG Hongwei, CHEN Xiaolong, CHEN Maozhang
doi: 10.7527/S1000-6893.2015.0144
2015, (8): 2544-2562.
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Some problems and thoughts in the development of aero-engine fan/compressor
LIU Yongquan, LIU Taiqiu, JI Luchen
doi: 10.7527/S1000-6893.2015.0078
2015, (8): 2563-2576.
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Overview of pathogen transmission in civil aircraft cabins
WANG Guangqiu, JI Shengcheng
doi: 10.7527/S1000-6893.2015.0145
2015, (8): 2577-2587.
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Impulsively starting flow problem: from incompressible to hypersonic flow
WU Ziniu, BAI Chenyuan, XU Shanshu, LI Juan, LIN Jing, CHEN Zijun, YAO Yao
doi: 10.7527/S1000-6893.2015.0147
2015, (8): 2588-2600.
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Effects of plug rear-body film cooling on infrared radiation and aerodynamic performance of axisymmetric plug nozzle
ZHANG Jingzhou, WANG Xu, SHAN Yong
doi: 10.7527/S1000-6893.2015.0119
2015, (8): 2601-2608.
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Progress review of satellite micro-vibration and control
MENG Guang, ZHOU Xubin
doi: 10.7527/S1000-6893.2015.0169
2015, (8): 2609-2619.
PDF [ 4320 K ]( 1058 ) HTML
Loading rate effect on interlaminar fracture toughness
LI Yulong, LIU Huifang
doi: 10.7527/S1000-6893.2015.0148
2015, (8): 2620-2650.
PDF [ 6942 K ]( 636 ) HTML
Research progress and application prospects of fan-wing aircraft
MENG Lin, YE Yongqiang, LI Nan
doi: 10.7527/S1000-6893.2015.0058
2015, (8): 2651-2661.
PDF [ 2664 K ]( 736 ) HTML
Integrated layout and topology optimization design of multi-component systems with assembly units
ZHANG Weihong, GUO Wenjie, ZHU Jihong
doi: 10.7527/S1000-6893.2015.0141
2015, (8): 2662-2669.
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A substructure method for coupling impulse response functions with finite element models via rigid-elastic joints
LIU Li, CHEN Shulin, ZHOU Sida, CHEN Zhaoyue
doi: 10.7527/S1000-6893.2015.0142
2015, (8): 2670-2680.
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Topology optimization of flexible support structure for trailing edge
JIN Dongping, JI Bin
doi: 10.7527/S1000-6893.2015.0105
2015, (8): 2681-2687.
PDF [ 2369 K ]( 819 ) HTML
Probabilistic fatigue life prediction method and modeling for complex structural parts
XIE Liyang, REN Jungang, WU Ningxiang, QIAN Wenxue
doi: 10.7527/S1000-6893.2015.0109
2015, (8): 2688-2695.
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Several hot issues and challenges in terminal guidance of flight vehicles
YAO Yu, ZHENG Tianyu, HE Fenghua, WANG Long, WANG Yang, ZHANG Xi, ZHU Baiyang, YANG Baoqing
doi: 10.7527/S1000-6893.2015.0176
2015, (8): 2696-2716.
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Challenge of control theory in the presence of high performance aircraft development
SHI Zhongke
doi: 10.7527/S1000-6893.2015.0155
2015, (8): 2717-2734.
PDF [ 2398 K ]( 717 ) HTML
Concept and architecture for new generation aircraft mission system
WANG Guoqing, GU Qingfan, WU Jianmin, WANG Miao
doi: 10.7527/S1000-6893.2015.0130
2015, (8): 2735-2752.
PDF [ 8173 K ]( 854 ) HTML
Identification and prediction of air traffic congestion
XU Xiaohao, LI Shanmei
doi: 10.7527/S1000-6893.2015.0123
2015, (8): 2753-2763.
PDF [ 1297 K ]( 557 ) HTML
Design of analytical prediction-correction skip entry guidance law based on matched asymptotic expansions
CUI Naigang, HUANG Rong, FU Yu, HAN Pengxin
doi: 10.7527/S1000-6893.2015.0143
2015, (8): 2764-2772.
PDF [ 1798 K ]( 399 ) HTML
Progress on manufacturing technology and process theory of aircraft composite structure
GU Yizhuo, LI Min, LI Yanxia, WANG Shaokai, ZHANG Zuoguang
doi: 10.7527/S1000-6893.2015.0156
2015, (8): 2773-2797.
PDF [ 9297 K ]( 1412 ) HTML
Filling rules in thin-walled and ribbed conical ring rolling for TC4 titanium alloy
GUO Lianggang, YANG He, DI Weijia, CHEN Fulong, ZHU Shuai
doi: 10.7527/S1000-6893.2015.0150
2015, (8): 2798-2806.
PDF [ 4332 K ]( 333 ) HTML
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