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Investigations on fidelity of high order accurate numerical simulation for computational fluid dynamics
Zhang Hanxin
2016, 34(1): 1-4. DOI: 10.7638/kqdlxxb-2015.0211
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Aerodynamic force/heating measurement on hypersonic vehicle across different flow regions
Yang Yanguang, Li Ming, Li Zhonghua, Li Xuguo, Dai Jinwen
2016, 34(1): 5-13. DOI: 10.7638/kqdlxxb-2015.0149
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Wind tunnel based virtual flight testing of aerodyanmics, flight dynamics and flight control for high maneuver missle
Zhao Zhongliang, Wu Junqiang, Li Hao, Zhou Weiqun, Mao Daiyong, Xiang Guangwei
2016, 34(1): 14-19. DOI: 10.7638/kqdlxxb-2015.0128
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The thrust vectoring experiment technique in the 2.4 m×2.4 m transonic wind tunnel
Li Jianqiang, Li Yaohua, Guo Danping, Miao Lei, Du Ning, Huang Cundong, Zhou Hong, Zeng Liquan, Zhang Yi
2016, 34(1): 20-26. DOI: 10.7638/kqdlxxb-2015.0131
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The effect and processing method for the lateral flexible angle in the angle of attack and roll coupled wind tunnel test
Xie Feng, Zhang Jiang, Qin Yongming
2016, 34(1): 27-32. DOI: 10.7638/kqdlxxb-2015.0115
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Wind tunnel test research on weapon bay cavity active flow control for acoustic
Song Wencheng, Li Yujun, Feng Qiang
2016, 34(1): 33-39. DOI: 10.7638/kqdlxxb-2015.0126
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Investigation on gust response test apparatus in FL-13 wind tunnel
Jin Hua, Wang Hui, Zhang Haiyou, Chen Peng, Yang Yuanzhi
2016, 34(1): 40-46. DOI: 10.7638/kqdlxxb-2015.0134
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Experimental investigation on boundary layer transition induced by distributed roughness elements
Wang Meng, Zhong Hongjie, Zhao Ronghuan
2016, 34(1): 47-53,69. DOI: 10.7638/kqdlxxb-2015.0102
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Experimental technique for micro rolling aerodynamics of a maneuvering reentry body
Zhao Junbo, Liang Bin, Fu Zengliang, Zhang Shiyu, Gao Qing
2016, 34(1): 53-58. DOI: 10.7638/kqdlxxb-2015.0037
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Formal design of experiments method of MDOE in wind tunnel tests
Zhang Jiang, Qin Yongming, Ma Handong
2016, 34(1): 59-69. DOI: 10.7638/kqdlxxb-2015.0116
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Research status and application of videogrammetric measurement techniques for wind tunnel testing
Zhang Zhengyu, Huang Xuhui, Yin Jiang, Zhou Run, Li Duo
2016, 34(1): 70-79. DOI: 10.7638/kqdlxxb-2015.0145
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Invetigation of skin-friction measurements using oil-film interferometry on airfoil wall in low speed wind tunnel
Geng Zihai, Shi Zhiwei, Jin Qigang
2016, 34(1): 80-85. DOI: 10.7638/kqdlxxb-2015.138
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Experimental investigation on lifting body aerodynamic force with simulated aft-body jet
Xu Xiaobin, Shu Haifeng, Xu Yun, Xie Fei, Sun Peng
2016, 34(1): 86-90. DOI: 10.7638/kqdlxxb-2015.148
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Application of phased array technique in the research of civil airplane airframe noise
Zhou Jiajian, Hao Xuan, Zhang Weimin, Chen Dabin
2016, 34(1): 91-97. DOI: 10.7638/kqdlxxb-2015.063
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Investigation on the interference correction of flying wing aircraft rear sting support in high speed wind tunnel test
Yi Bingli, Zeng Kai, Wang Shihong
2016, 34(1): 98-106. DOI: 10.7638/kqdlxxb-2015.0098
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Investigation on the correlation of high-speed force test results of flying-wing calibration model with low-aspect ratio
Li Yonghong, Liu Huilong, Huang Yong, Zhong Shidong, Su Jichuan
2016, 34(1): 107-113,130. DOI: 10.7638/kqdlxxb-2015.0096
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Three types of transonic wind tunnel wall interference correction method and their application on low aspect ratio flying wing calibration model
Zhong Shidong, Li Wei, Su Jichuan, Li Yonghong, He Zhong
2016, 34(1): 113-118. DOI: 10.7638/kqdlxxb-2015.0095
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Study on the distortion effect of flying wing in low speed wind tunnel
Jin Ling, Liu Litao, Zhu Minghong, Sun Chuanbao, Chen Lujun
2016, 34(1): 119-124. DOI: 10.7638/kqdlxxb-2015.0094
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Low speed experiment on longitudinal and lateral aerodynamic characteristics of the low aspect ratio flying wing calibration model
Wu Junfei, Qin Yongming, Huang Zhan, Wei Zhongwu, Jia Yi
2016, 34(1): 125-130. DOI: 10.7638/kqdlxxb-2015.0093
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Transonic porous wall interference characteristics of the low aspect ratio flying wing model in FL-2 wind tunnel
Li Hongyan, Wang Xiangyun, Yang Ximing, Wang Shihong
2016, 34(1): 131-137. DOI: 10.7638/kqdlxxb-2015.0091
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