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Engineering calculation of non-equilibrium effects on thermal environment of reentry vehicles
Guo Yijun, Dai Guangyue, Gui Yewei, Tong Fulin, Qiu Bo, Liu Xiao
2015, 33(5): 581-587. DOI: 10.7638/kqdlxxb-2014.0041
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Aerodynamic configuration design optimization of reentry capsule based on CFD and multi-objective optimization theory
Wang Rong, Chen Bingyan
2015, 33(5): 588-593,609. DOI: 10.7638/kqdlxxb-2014.0045
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Numerical research of NASA high-lift trap wing model based on HyperFLOW
Zhao Zhong, He Xin, Zhang Laiping, He Kun, He Lei
2015, 33(5): 594-602. DOI: 10.7638/kqdlxxb-2014.0026
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Effects of compressibility correction on γ-Reθ transition model
Xia Chenchao, Jiang Tingting, Guo Zhongzhou, Chen Weifang
2015, 33(5): 603-609. DOI: 10.7638/kqdlxxb-2014.0068
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Inverse design method for the Licher biplane with a new target pressure distribution
Zhao Chengxi, Ye Zhengyin, Hua Ruhao
2015, 33(5): 610-616,630. DOI: 10.7638/kqdlxxb-2014.0040
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Numerical prediction method of aerodynamic noise including boundary scattering generated by high subsonic cavity flow
Wang Fang, Liu Qiuhong, Cai Jinsheng
2015, 33(5): 617-623. DOI: 10.7638/kqdlxxb-2015.0004
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Multi-block patched mesh in gas-kinetic unified algorithm
Wu Junlin, Peng Aoping, Li Zhihui, Fang Ming
2015, 33(5): 624-630. DOI: 10.7638/kqdlxxb-2014.0016
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Three-dimensional numerical simulations for transonic axial compressors using a mixing plane method
Zhang Jian, Tang Zhigong, Deng Youqi, Zhou Naichun
2015, 33(5): 631-635. DOI: 10.7638/kqdlxxb-2014.0019
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Numerical analyses of vortex structure induced by dimple
Liu Jing, Li Jie, Jiang Shengju
2015, 33(5): 636-642. DOI: 10.7638/kqdlxxb-2014.0030
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DDES of aeroacoustic over an open cavity with and without a spoiler
Liu Yu, Tong Mingbo, Zhiwei Hu
2015, 33(5): 643-648. DOI: 10.7638/kqdlxxb-2014.0025
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Unsymmetrical aerodynamic derivatives of hypersonic free-flight spinning cone
Jiang Zenghui, Song Wei, Chen Nong
2015, 33(5): 649-654,660. DOI: 10.7638/kqdlxxb-2014.0033
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Investigation on lift stall characteristics of propeller aircraft
Liu Yi, Zhao Xiaoxia, Ouyang Shaoxiu
2015, 33(5): 655-660. DOI: 10.7638/kqdlxxb-2014.0024
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Ablation test technique of large scale structure component in arc-heated wind tunnel
Ou Dongbin, Chen Lianzhong, Dong Yonghui, Peng Jinlong, Chen Feng
2015, 33(5): 661-666. DOI: 10.7638/kqdlxxb-2014.0017
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Experiment on static aeroelastic in high speed wind tunnel
Yang Xianwen, Yu Li, Lyu Binbin, Guo Hongtao, Yang Zhenhua, Kou Xiping
2015, 33(5): 667-672. DOI: 10.7638/kqdlxxb-2014.0018
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Flush static ports placement on a commercial transport aircraft: a design practice from aerodynamic perspectives
Sun Yifeng, Yang Shipu, Fang Yang, Chen Yingchun
2015, 33(5): 673-677. DOI: 10.7638/kqdlxxb-2014.0021
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Buffeting control of the free-standing tower of a super-long-span cable-stayed bridge using MTMD
Tao Tianyou, Wang Chunfeng, Wang Hao, Li Aiqun
2015, 33(5): 678-685. DOI: 10.7638/kqdlxxb-2014.0023
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Numerical research on basic characteristics of tunnel entry waves induced by a high-speed train running into the tunnel
Mei Yuangui, Zhang Chengyu, Xu Jianlin, Li Shi'an, Hao Lei
2015, 33(5): 686-696. DOI: 10.7638/kqdlxxb-2013.0082
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Wind tunnel test and numerical simulation study on internal wind loading for super large cooling tower
Zou Yunfeng, He Xuhui, Chen Zhengqing, Niu Huawei
2015, 33(5): 697-705. DOI: 10.7638/kqdlxxb-2013.0084
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Numerical method for identifying the aerodynamic admittance of bridge deck
Tang Yu, Zheng Shixiong, Zhang Longqi, Ma Cunming, Gu Hongqiang
2015, 33(5): 706-713. DOI: 10.7638/kqdlxxb-2014.0079
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Numerical simulation of the effect of the permeability on the ringsail parachute in terminal descent stage
Yang Xue, Yu Li, Li Yunwei, Li Yanjun
2015, 33(5): 714-719. DOI: 10.7638/kqdlxxb-2014.0081
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