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25 December 2011, Volume 32 Issue 12

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25 December 2011, Volume 32 Issue 12

Articles

A Two-step Optimization Method of Transonic Wing Design for Engineering Application
Abstract( 2355 )

LI Peifeng, ZHANG Binqian, CHEN Yingchun

doi: CNKI:11-1929/ V.20110823.1119.002

2011, (12): 2153-2162.

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Nonlinear Dynamics of Static Stall of Airfoil and Its Control
Abstract( 2614 )

ZHANG Jiazhong, LI Kailun, CHEN Liying

doi: CNKI:11-1929/V.20110726.1650.004

2011, (12): 2163-2173.

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Weaving Maneuver Trajectory Design for Hypersonic Glide Vehicles
Abstract( 3483 )

XIE Yu, LIU Luhua, TANG Guojian, XU Mingliang

doi: CNKI:11-1129/V.20110921.0830.001 *通讯作者.Tel.: 0731-84573140 E-mail: gjtang@263.net

2011, (12): 2174-2181.

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Pressure Controlled Vortex Design of 1.5-stage Turbine Based on the Method of Controlling Axial Velocity Variation
Abstract( 2698 )

DENG Qingfeng, ZHENG Qun, LIU Chunlei, LI Song

doi: CNKI: 11-1929/V.20110615.1322.003

2011, (12): 2182-2193.

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Research on Hazard Identification of Turbo-fan Engine Digital Control Systems Based on Functional Hazard Analysis
Abstract( 2674 )

GONG Lei, ZHANG Shuguang, LIU Xiaofeng, QIU Tian

doi: CNKI:11-1929/V.20110831.1320.001

2011, (12): 2194-2203.

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Prediction of Aeroacoustic Noise for Helicopter Rotors Based on Vorticity Confinement Method
Abstract( 3511 )

XU Jianhua, SONG Wenping, HAN Zhonghua

doi: CNKI:11-1929/V.20110906.1123.002

2011, (12): 2204-2212.

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E-Bayes Reliability Analysis for Liquid Rocket Engine with Zero-failure Data
Abstract( 2520 )

HAN Ming

doi: CNKI:11-1929/V.20110616.1730.003

2011, (12): 2213-2219.

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Numerical Model Development and Validation for Hydrocarbon Fuel Supercritical Heat Transfer with Endothermic Pyrolysis
Abstract( 2849 )

RUAN Bo, MENG Hua

doi: CNKI:11-1929/V.20110627.1733.003

2011, (12): 2220-2226.

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Analysis of Influence of Aircraft Flexibility on Nose Landing Gear Shimmy
Abstract( 3461 )

FENG Fei, CHANG Zheng, NIE Hong, ZHANG Ming, PENG Yiming

doi: CNKI:11-1929/V.20110726.1649.003

2011, (12): 2227-2235.

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An Approach for Vibration Analysis of Continuous Systems with Piecewise-linear Boundary Conditions
Abstract( 2458 )

WEI Hongtao, KONG Xianren, WANG Benli, ZHANG Xiangmeng

doi: CNKI:11-1929/V.20110831.1320.003

2011, (12): 2236-2243.

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Study of Satellite Relative Motion in Elliptical Orbit Using Relative Orbit Elements
Abstract( 1995 )

HAN Chao, YIN Jianfeng

doi: CNKI:11-1929/V.20110823.1119.001

2011, (12): 2244-2258.

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Flight Controller Design Using Adaptive Parameter Approximation Block Backstepping
Abstract( 3844 )

CAO Lijia, ZHANG Shengxiu, LIU Yi'nan, LIU Ying, ZHANG Ying

doi: CNKI:11-1929/V.20111018.1013.001

2011, (12): 2259-2267.

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A Method of Detecting Differential Frequency Hopping Signal Based on Multiple-hop Autocorrelation
Abstract( 2172 )

QIAN Bo, FENG Yongxin, PAN Chengsheng, TIAN Minghao

doi: CNKI:11-1929/ V.20110810.1118.002

2011, (12): 2268-2276.

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Fault Injection Method Resulting from Inaccessible Location Fault Based on Fault Propagation Characteristics
Abstract( 2547 )

LI Tianmei, HU Changhua, ZHOU Xin

doi: CNKI: 11-1929/V.20110627.1733.002

2011, (12): 2277-2286.

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Joint DOD and DOA Estimation for MIMO Radar with Electromagnetic Vector Sensors
Abstract( 3910 )

WANG Kerang, HE Yapeng, ZHU Xiaohua

doi: CNKI:11-1929/V.20110815.1716.002

2011, (12): 2287-2292.

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Optimization Model and Algorithm for Aircraft Scheduling Problem Based on Cooperative Multi-task Assignment
Abstract( 2500 )

ZHOU Kun, XIA Hongshan

doi: CNKI:11-1929/V.20110815.1716.003

2011, (12): 2293-2302.

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Passivity Design for the Control Loading System of a Flight Simulator
Abstract( 2519 )

LIU Yanwen, WANG Guangxiong, LI Jia

doi: CNKI:11-1929/V.20110526.1757.023

2011, (12): 2303-2309.

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Motion State Estimation for Micro UAV Using Inertial Sensor and Stereo Camera Pair
Abstract( 2000 )

LI Jian, LI Xiaomin, QIAN Kechang, ZHOU Hongxin

doi: CNKI:11-1929/V.20110727.0907.002

2011, (12): 2310-2317.

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Influence of Rover Unloading on Lunar Lander Stability
Abstract( 1852 )

DENG Zongquan, LI Kui, LIU Rongqiang, JIANG Shengyuan

doi: CNKI:11-1929/V.20110620.1341.002

2011, (12): 2318-2326.

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Optimal Design of Isotropy Performance of Six-dimensional Force Sensor Based on Standard Stewart Parallel Structure Lying on a Circular Hyperboloid of One Sheet
Abstract( 2614 )

TONG Zhizhong, JIANG Hongzhou, HE Jingfeng, DUAN Guangren

doi: CNKI:11-1929/V.20110726.1649.002

2011, (12): 2327-2334.

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Fabrication and Performance Evaluation of Micro-channels in Aircraft Wind-tunnel-models for Pressure Measurements Using Stereolithography
Abstract( 3364 )

ZHANG Wei, LI Dichen, ZHAO Xinglei, ZHU Weijun, WANG Wei, LIU Jun

doi: CNKI:11-1929/V.20110620.1341.003

2011, (12): 2335-2340.

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