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Development of hypersonic flow research in China based on supported projects of NSFC
ZHANG Panfeng, ZHAN Shige
doi: 10.7527/S1000-6893.2014.0222
2015, (1): 1-6.
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Some aerodynamic issues in hypersonic flight
YU Ping, DUAN Yi, CHEN Jun
doi: 10.7527/S1000-6893.2014.0224
2015, (1): 7-23.
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A comprehensive analysis of aerodynamics for spacecraft re-entery Earth's atmosphere surroundings
FANG Fang, ZHOU Lu, LI Zhihui
doi: 10.7527/S1000-6893.2014.0225
2015, (1): 24-38.
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Inspiration of hypersonic vehicle with airframe/propulsion integrated design
LUO Jinling, LI Chao, XU Jin
doi: 10.7527/S1000-6893.2014.0226
2015, (1): 39-48.
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Difficulties in aerodynamic design problems of the winged hypersonic reentry vehicle
YANG Yong, ZHANG Hui, ZHENG Hongtao
doi: 10.7527/S1000-6893.2014.0227
2015, (1): 49-57.
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Analysis of flow characteristics for hypersonic vehicle
WU Ziniu, BAI Chenyuan, LI Juan, CHEN Zijun, JI Shixiang, WANG Dan, WANG Wenbin, XU Yizhe, YAO Yao
doi: 10.7527/S1000-6893.2014.0228
2015, (1): 58-85.
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Research progress on hypersonic wind tunnel aerodynamic testing techniques
TANG Zhigong, XU Xiaobin, YANG Yanguang, LI Xuguo, DAI Jinwen, LYU Zhiguo, HE Wei
doi: 10.7527/S1000-6893.2014.0229
2015, (1): 86-97.
PDF [ 3848 K ]( 787 ) HTML
Progress on experimental techniques and studies of hypersonic/supersonic flows
YI Shihe, CHEN Zhi, ZHU Yangzhu, HE Lin, WU Yu
doi: 10.7527/S1000-6893.2014.0230
2015, (1): 98-119.
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More fidelity, more accurate, more efficient—progress on numerical simulations for hypersonic flow
TANG Zhigong, ZHANG Yirong, CHEN Jianqiang, MAO Meiliang, ZHANG Yifeng, LIU Huayong
doi: 10.7527/S1000-6893.2014.0231
2015, (1): 120-134.
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Gas kinetic scheme in hypersonic flow simulation
XU Kun, CHEN Songze
doi: 10.7527/S1000-6893.2014.0232
2015, (1): 135-146.
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Direct numerical simulation techniques for hypersonic turbulent flows
LI Xinliang
doi: 10.7527/S1000-6893.2014.0233
2015, (1): 147-158.
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Progress in numerical simulation techniques of hypersonic aerodynamic problems
WANG Jiangfeng, WU Yizhao, JI Weidong, FAN Xiaofeng, ZHAO Faming, LYU Zhenjun
doi: 10.7527/S1000-6893.2014.0214
2015, (1): 159-175.
PDF [ 10192 K ]( 988 ) HTML
Problems of numerical simulation of high-temperature gas flow fields for hypersonic vehicles
LI Haiyan, TANG Zhigong, YANG Yanguang, SHI Anhua, LUO Wanqing
doi: 10.7527/S1000-6893.2014.0235
2015, (1): 176-191.
PDF [ 12708 K ]( 1246 ) HTML
Influence analysis of hypersonic flight vehicle model uncertainty
YU Jia, YANG Pengfei, YAN De
doi: 10.7527/S1000-6893.2014.0221
2015, (1): 192-200.
PDF [ 4304 K ]( 841 ) HTML
A massively parallel algorithm for hypersonic covering various flow regimes to solve Boltzmann model equation
LI Zhihui, WU Junlin, JIANG Xinyu, MA Qiang
doi: 10.7527/S1000-6893.2014.0219
2015, (1): 201-212.
PDF [ 11726 K ]( 576 ) HTML
Active control and nonlinear numerical simulation for oscillating pressure of high-speed aircraft cavity
WANG Yiding, Guo Liang, TONG Mingbo, Zhang Jie
doi: 10.7527/S1000-6893.2014.0277
2015, (1): 213-222.
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Aerodynamic characteristics analysis of air-breathing hypersonic vehicles at high angle of attack
LUO Wenli, LI Daochun, XIANG Jinwu
doi: 10.7527/S1000-6893.2014.0266
2015, (1): 223-231.
PDF [ 14747 K ]( 799 ) HTML
Internal flowpath for hypersonic ramjet based on subsonic combustion
DUAN Xihuai, ZHENG Riheng, LI Lihan
doi: 10.7527/S1000-6893.2014.0236
2015, (1): 232-244.
PDF [ 10396 K ]( 814 ) HTML
Progress in airframe-propulsion integration technology of air-breathing hypersonic vehicle
WU Yingchuan, HE Yuanyuan, HE Wei, LE Jialing
doi: 10.7527/S1000-6893.2014.0238
2015, (1): 245-260.
PDF [ 29626 K ]( 24271 ) HTML
Modeling of turbulence-chemistry interactions in numerical simulations of supersonic combustion
YANG Yue, YOU Jiaping, SUN Mingbo
doi: 10.7527/S1000-6893.2014.0239
2015, (1): 261-273.
PDF [ 7397 K ]( 971 ) HTML
Research progress of hypersonic inlet reverse design based on curved shock compression system
ZHANG Kunyuan
doi: 10.7527/S1000-6893.2014.0240
2015, (1): 274-288.
PDF [ 22848 K ]( 414 ) HTML
Integrated design of forebody and inlet based on external and internal conical basic flow field with controlled Mach number distribution surface
LI Yongzhou, ZHANG Kunyuan
doi: 10.7527/S1000-6893.2014.0263
2015, (1): 289-301.
PDF [ 16056 K ]( 709 ) HTML
Flow characteristics experiments of a hypersonic axisymmetric inlet with nose bluntness
GAO Wenzhi, LI Zhufei, YANG Jiming
doi: 10.7527/S1000-6893.2014.0259
2015, (1): 302-310.
PDF [ 8519 K ]( 537 ) HTML
Numerical study of coupled surface temperature distribution and aerodynamic heat for hypersonic vehicles
DONG Weizhong, GAO Tiesuo, DING Mingsong, JIANG Tao, LIU Qingzong
doi: 10.7527/S1000-6893.2014.0241
2015, (1): 311-324.
PDF [ 12531 K ]( 1845 ) HTML
Hypersonic aeroheating prediction technique and its trend of development
PENG Zhiyu, SHI Yilei, GONG Hongming, LI Zhonghua, LUO Yicheng
doi: 10.7527/S1000-6893.2014.0242
2015, (1): 325-345.
PDF [ 20003 K ]( 19127 ) HTML
Multidisciplinary dynamics modeling and analysis of a generic hypersonic vehicle
HUA Ruhao, YE Zhengyin
doi: 10.7527/S1000-6893.2014.0243
2015, (1): 346-356.
PDF [ 4544 K ]( 821 ) HTML
Transition and prediction for hypersonic boundary layers
LUO Jisheng
doi: 10.7527/S1000-6893.2014.0244
2015, (1): 357-372.
PDF [ 18237 K ]( 1481 ) HTML
Operational identification of time-varying modal parameters for thermal structures of high-speed aerial vehicles
ZHOU Sida, LIU Li, LI Yulin, ZHOU Xiaochen
doi: 10.7527/S1000-6893.2014.0267
2015, (1): 373-380.
PDF [ 9870 K ]( 612 ) HTML
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