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The PSE approach to study the nonlinear evolution of three-dimensional disturbances in incompressible boundary layers on flat-plate
Zhang Li
2015, 33(4): 441-445. DOI: 10.7638/kqdlxxb-2014.0022
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Adaptive discontinuous Galerkin method to solve Euler equations based on high-order approximative boundary
Sun Qiang, Lv Hongqiang, Wu Yizhao
2015, 33(4): 446-453. DOI: 10.7638/kqdlxxb-2014.0027
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Highly-efficient CFD calculations on viscous flow of hovering rotor based on the implicit algorithm
Wu Qi, Zhao Qijun, Zhao Guoqing, Wang Bo
2015, 33(4): 454-463. DOI: 10.7638/kqdlxxb-2014.0035
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Application research of TSP technique in transition detection
Shang Jinkui, Wang Peng, Chen Liusheng, Zhong Hongjie, Zhao Min
2015, 33(4): 464-469. DOI: 10.7638/kqdlxxb-2014.0034
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Research Reynolds number effect correction for air supercritical laminar complex wing
Feng Wenliang, Chen Bin, Lyu Lingying
2015, 33(4): 470-474. DOI: 10.7638/kqdlxxb-2013.0086
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Numerical research on lateral jet interaction for a canard missile rolling control
Zhou Peipei
2015, 33(4): 475-480. DOI: 10.7638/kqdlxxb-2013.0098
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CFD computation and POD analysis for transonic buffet on a supercritical airfoil
Dong Shenghua, Shi Aiming, Ye Zhengyin, Tian Haitao
2015, 33(4): 481-487. DOI: 10.7638/kqdlxxb-2013.0100
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Experimental study on flush airdata sensing system calibration in wind tunnel
Qin Yongming, Zhang Chun, Dong Jingang
2015, 33(4): 488-492.
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Numerical investigations of a tandem stator stage for a small turbo-shaft engine
Wei Wei, Liu Bo
2015, 33(4): 493-500. DOI: 10.7638/kqdlxxb-2013.0105
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Research on aerodynamic configuration design principle for advanced hypersonic vehicle
Du Tao, Chen Yu, Cai Qiaoyan, Wu Yansen
2015, 33(4): 501-509. DOI: 10.7638/kqdlxxb-2013.0106
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The research on the aerodynamic and structural characteristics of elliptic cross section of variable parameters
Liu Yi, Li Yang, Zhao Xiaoxia
2015, 33(4): 510-514. DOI: 10.7638/kqdlxxb-2013.0110
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Slat cove filler design for noise reduction based on artificial neural network
Tao Jun, Sun Gang, Xu Kangle
2015, 33(4): 515-522. DOI: 10.7638/kqdlxxb-2013.0111
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Aerodynamic noise source detection for main landing gear based on phased microphone array technique
Xu Kangle, Chen Yingchun, Jiang Yuan, Zhou Jiajian, Sun Gang
2015, 33(4): 523-529. DOI: 10.7638/kqdlxxb-2013.0112
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Fast prediction based on effective numerical method for aerodynamic force and heat of high speed vehicles
Wang Rong, Zhang Xuejun, Ji Chuqun
2015, 33(4): 530-535. DOI: 10.7638/kqdlxxb-2014.0003
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Numerical simulation of ice shedding from civil airplane nose
Feng Lijuan, Tan Guangkun, Zhang Qiang, Yi Xian
2015, 33(4): 536-541. DOI: 10.7638/kqdlxxb-2014.0005
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An identification study on the added mass and aerodynamic damping based on Hilbert-Huang Transform under the action of fluctuating wind
Sun Xufeng, Hu Chao
2015, 33(4): 542-547.
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Utility helicopter design synthesison of stealth and aerodynamic configuration
Bao Xiaoxiang, Zhang Yunfei, Yang Xiaoshu
2015, 33(4): 548-553. DOI: 10.7638/kqdlxxb-2014.0012
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Numerical simulation study on propeller slipstream effect on unmanned air vehicle with propeller engine
Chen Guangqiang, Bai Peng, Zhan Huiling, Ji Chuqun
2015, 33(4): 554-562. DOI: 10.7638/kqdlxxb-2014.0013
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An overlapping grid adaptive interface advancement method for hypersonic continuum-rarefied flow and its application
Xu Xiao, Wang Xuede, Huang Fei, Tang Junjie
2015, 33(4): 563-571. DOI: 10.7638/kqdlxxb-2014.0015
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Study on wind pressure distribution and gust response coefficient for a new terminal
Peng Liuliu, Huang Guoqing, Li Mingshui, Yuan Liming, Luo Nan
2015, 33(4): 572-579. DOI: 10.7638/kqdlxxb-2014.0014
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