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Applications of discontinuous Galerkin method in numerical simulations of compressible flows:A review
LYU Hongqiang, ZHANG Tao, SUN Qiang, CHEN Jianwei, QIN Wanglong
2017, 35(4): 455-471. DOI: 10.7638/kqdlxxb-2017.0051
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Developments of aeroacoustic investigation on high-lift device for large aircrafts
LIU Peiqing, LI Ling, XING Yu, GUO Hao
2017, 35(4): 472-484. DOI: 10.7638/kqdlxxb-2017.0066
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Applications of counterflowing jet technology in hypersonic vehicle
DENG Fan, XIE Feng, HUANG Wei, ZHANG Dong, JIAO Zihan, CHEN Jun, LIU Sen
2017, 35(4): 485-495. DOI: 10.7638/kqdlxxb-2017.0057
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Investigation on aerothermodynamic environment and ablation which lead to HTV-2 second fight test failing
GUO Yijun, ZENG Lei, ZHANG Haoyuan, DAI Guangyue, WANG Anling, QIU Bo, ZHOU Shuguang, LIU Xiao
2017, 35(4): 496-503. DOI: 10.7638/kqdlxxb-2016.0114
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Numerical and experimental investigation on aerodynamic characteristics for one typical near space vehicle
LI Qian, ZHAO Zhongliang, YE Youda, TAO Yang, MA Shang, LI Yuping, WANG Xiaobing
2017, 35(4): 504-509. DOI: 10.7638/kqdlxxb-2016.0116
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Numerical study on local separation flow over body flaps of hypersonic vehicle
SHI Lei, GONG Anlong, YANG Yunjun, ZHOU Weijiang
2017, 35(4): 510-515. DOI: 10.7638/kqdlxxb-2015.0192
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Aerodynamic shape design methods for aircraft:status and trends
GAO Zhenghong, WANG Chao
2017, 35(4): 516-528. DOI: 10.7638/kqdlxxb-2017.0058
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Evolution and development of "man-in-loop" in aerodynamic optimization design
LI Runze, ZHANG Yufei, CHEN Haixin
2017, 35(4): 529-543. DOI: 10.7638/kqdlxxb-2017.0076
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Aerodynamic optimization analyses of tiltrotor/propeller based on CFD method
ZHAO Qijun, JIANG Shuang, LI Peng, WANG Bo, ZHANG Hang
2017, 35(4): 544-553. DOI: 10.7638/kqdlxxb-2017.0061
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Investigation of gradient computation based on discrete adjoint method
HUANG Jiangtao, LIU Gang, ZHOU Zhu, GAO Zhenghong, HUANG Yong
2017, 35(4): 554-562. DOI: 10.7638/kqdlxxb-2017.0064
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Study on a new RLV lifting body concept and its aerodynamic configuration optimization design
FENG Yi, LIU Shenshen, LU Fengshun, TANG Wei, HUANG Yong, SUN Junfeng, GUI Yewei
2017, 35(4): 563-571. DOI: 10.7638/kqdlxxb-2017.0067
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Multi-objective optimization of Fowler flap on general aircraft
WEI Chuang, ZHANG Tiejun, LIU Tiezhong
2017, 35(4): 572-578. DOI: 10.7638/kqdlxxb-2017.0070
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Study on supercritical airfoil of blended wing body
LI Quan, GUO Zhaodian, LEI Wutao, ZHAO Ke
2017, 35(4): 579-586. DOI: 10.7638/kqdlxxb-2017.0073
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Multidisciplinary optimization design of high dimensional target space for flying wing airfoil
ZHENG Chuanyu, HUANG Jiangtao, ZHOU Zhu, LIU Gang, GAO Zhenghong, XU Yong
2017, 35(4): 587-597. DOI: 10.7638/kqdlxxb-2017.0079
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Aerodynamic/structural integrated design for aircraft wing with static aeroelasticity effect
YANG Tihao, BAI Junqiang, XIN Liang, SUN Zhiwei, SHI Yayun
2017, 35(4): 598-609. DOI: 10.7638/kqdlxxb-2017.0082
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