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Display Method:
Progress in observational studies of aircraft wake vortex in ground proximity
PAN Weijun, LUAN Tian, KANG Xianbiao, ZHANG Qingyu, REN Jie, ZHANG Qiang
2019, 37(4): 511-521. DOI: 10.7638/kqdlxxb-2018.0136
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Numerical study on cross-flow transition in three-dimensional hypersonic boundary layers
HAN Yufeng, MA Shaoxian, SU Caihong
2019, 37(4): 522-529. DOI: 10.7638/kqdlxxb-2019.0015
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Assessment of SAS and PANS models in simulations of flow over a circular cylinder
LIU Yue, GUAN Xiaorong, XU Cheng
2019, 37(4): 530-540. DOI: 10.7638/kqdlxxb-2017.0072
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An adaptive high-resolution hybrid scheme using central flux scheme and WENO scheme
TIAN Qi, GUO Yuan, LIANG Xian, LI Xinliang
2019, 37(4): 541-545, 577. DOI: 10.7638/kqdlxxb-2017.0050
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Massive parallel program design for unsteady full annulus turbomachine simulation
ZHANG Jian, TANG Jing, QIU Ming, DENG Youqi, GONG Xiaoquan
2019, 37(4): 546-554. DOI: 10.7638/kqdlxxb-2017.0065
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Study on three-dimensional effect correction of surface heat flux estimation based on neural network
PAN Xuehao, CHEN Weifang, PENG Yuzhuo, YANG Hua
2019, 37(4): 555-562. DOI: 10.7638/kqdlxxb-2017.0069
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Constrained estimation method of thermal conductivity of a material
ZHOU Yu, QIAN Weiqi, SHAO Yuanpei, YAN Weixu
2019, 37(4): 563-568. DOI: 10.7638/kqdlxxb-2017.0080
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Study on improvement of low speed pitching moment characteristics of civil aircraft
ZHONG Yuan, YANG Xiaoquan, LIU Kaili, WU Dawei, SI Jiangtao
2019, 37(4): 569-577. DOI: 10.7638/kqdlxxb-2017.0097
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Influence investigation of engine exhaust on aerodynamic performance for the flying wing UAV
ZHANG Xiang, CAO Deyi, HE Haibo, CUI Fei
2019, 37(4): 578-585. DOI: 10.7638/kqdlxxb-2017.0052
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Fast response pressure-sensitive paint measurement of transonic cascades
ZHANG Xue, ZHONG Hongjie, WANG Meng, ZHAO Min
2019, 37(4): 586-592, 599. DOI: 10.7638/kqdlxxb-2017.0031
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Development and flight testing of a fluidic thrust vectoring demonstrator
CAO Yongfei, GU Yunsong, HAN Jiexing
2019, 37(4): 593-599. DOI: 10.7638/kqdlxxb-2017.0202
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Progress and challenges of sonic boom research
QIAN Zhansen, HAN Zhonghua
2019, 37(4): 601-619. DOI: 10.7638/kqdlxxb-2019.0054
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Key technologies for next-generation environmentally-friendly supersonic transport aircraft: a review of recent progress
HAN Zhonghua, QIAO Jianling, DING Yulin, WANG Gang, SONG Bifeng, SONG Wenping
2019, 37(4): 620-635. DOI: 10.7638/kqdlxxb-2018.0288
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Review of recent progress of wind tunnel measurement techniques for off-body sonic boom pressure
LIU Zhongchen, QIAN Zhansen, LENG Yan
2019, 37(4): 636-645. DOI: 10.7638/kqdlxxb-2018.0282
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Overview of sonic boom theory, prediction and minimization methods for supersonic civil aircraft
LAN Shilong
2019, 37(4): 646-654, 645. DOI: 10.7638/kqdlxxb-2018.0294
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Analysis on typical parameters of bodies of revolution affecting the sonic boom
LENG Yan, QIAN Zhansen, LIU Zhongchen
2019, 37(4): 655-662, 689. DOI: 10.7638/kqdlxxb-2018.0291
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Sonic boom prediction method for supersonic transports based on augmented Burgers equation
QIAO Jianling, HAN Zhonghua, DING Yulin, CHI Jiangbo, MENG Guanyu, SONG Bifeng, SONG Wenping
2019, 37(4): 663-674. DOI: 10.7638/kqdlxxb-2018.0267
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Flight measurement and numerical simulation of sonic boom signature of OS-X0 experimental aircraft
QIAN Zhansen, LIU Zhongchen, LENG Yan, ZHANG Xue, GAO Liangjie, DENG Fan
2019, 37(4): 675-682. DOI: 10.7638/kqdlxxb-2018.0276
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Application of Stevens' loudness in low-boom design of supersonic civil aircraft
WANG Yuhang, XU Yue
2019, 37(4): 683-689. DOI: 10.7638/kqdlxxb-2018.0285
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