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Vortex structures and mixing of compressible mixing layer
ZHOUQiang, HEFeng, SHENMengyu
2014, 32(3): 273-279. DOI: 10.7638/kqdlxxb-2013.0099
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Thermo-chemical nonequilibrium process in N2/N mixture with state-to-state model
XUDan, ZENGMing, ZHANGWei, LIUJun
2014, 32(3): 280-288. DOI: 10.7638/kqdlxxb-2012.0139
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Numerical simulation of unsteady propeller slipstream
YANGXiaochuan, WANGYuntao, WANGGuangxue, ZHANGYulun
2014, 32(3): 289-294. DOI: 10.7638/kqdlxxb-2012.0147
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Study on asymmetric flow over slender body at high angles of attack via Particle Image Velocimetry test in high speed wind tunnel
HEZhong, WUJunqiang, JIANGWeimin, WUJifei
2014, 32(3): 295-299. DOI: 10.7638/kqdlxxb-2012.0106
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Aerodynamic shape optimization and design of airfoils with low Reynolds number
CHENXuekong, GUOZheng, YIFan, WANGRuibo, LIUGuangyuan, LIHongxing
2014, 32(3): 300-306. DOI: 10.7638/kqdlxxb-2012.0134
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Large eddy stimulation and experimental measurement of near wake structures of a slotted circular cylinder
YANGJinwen, HEYi, BAOFeng
2014, 32(3): 308-314. DOI: 10.7638/kqdlxxb-2013.0033
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Measurement of pressure center of re-entry vehicle module
QINYongming, WEIZhongwu, DONGJingang, CHENQiang, ZHANGJiang
2014, 32(3): 315-319. DOI: 10.7638/kqdlxxb-2013.0039
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Numerical analysis of helicopter rotor/fuselage unsteady aerodynamic interaction
TANJianfeng, WANGHaowen
2014, 32(3): 320-327. DOI: 10.7638/kqdlxxb-2012.0141
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Aircraft jig shape design based on radial basis functions and Delaunay graphic mapping
HUANGJiangtao, GAOZhenghong, BAIJunqiang, ZHOUzhu, ZHAOKe
2014, 32(3): 328-333. DOI: 10.7638/kqdlxxb-2012.0099
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Numerical simulation of a grid fin missile based on structure grid
ZHOUPeipei
2014, 32(3): 334-338. DOI: 10.7638/kqdlxxb-2012.0100
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Nested grids using patched grid generation technique and characteristics computation of variable forwardswept wing
WANGXu, YUChong, SUXinbing, CHENPeng
2014, 32(3): 339-344. DOI: 10.7638/kqdlxxb-2012.0115
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Numerical simulation for two-dimensional unsteady moving boundary problems based on IBVCM
LUHaitian, WUJie, ZHAONing
2014, 32(3): 345-350. DOI: 10.7638/kqdlxxb-2012.0116
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Wind tunnel test on across-wind aerodynamic damping of rectangular super-high-rise buildings
CAOHuilan, QUANYong, GUMing
2014, 32(3): 351-359. DOI: 10.7638/kqdlxxb-2012.0119
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The primary study of 3-point calculation method for the flush air data system
LIQichang, LIUJinfan, LIUXin, YANGYicheng, CHENJianzhong, TIANPeizhou, YANGJie, KANGHongbo, ZHUShimin
2014, 32(3): 360-363. DOI: 10.7638/kqdlxxb-2012.0122
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Flutter characteristic simulation and experimental verification for transonic flutter model of a whole aircraft
QIANWei, YANGGuowei, ZHANGGuijiang, ZHENGGuannan
2014, 32(3): 364-368. DOI: 10.7638/kqdlxxb-2012.0123
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Prediction and analysis of flow oscillation modes inside open cavities at transonic or supersonic speeds
YANGDangguo, ZHUJing, 3, LIJianqiang, LIANGJinmin
2014, 32(3): 369-375. DOI: 10.7638/kqdlxxb-2012.0126
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Aerodynamic effects of supercooled large droplet runback ice on airfoils
LIYanxin, ZHANGChen, LIUHong, WANGFuxin
2014, 32(3): 376-382. DOI: 10.7638/kqdlxxb2012.0127
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Proportional side force control of slender body at high angles of attack with non-zero sideslip angle
ZHOUYuxiao, GUYunsong
2014, 32(3): 383-387. DOI: 10.7638/kqdlxxb-2012.0129
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Influence of model surface roughness on wind-induced response and interference of cooling tower
ZOUYunfeng, CHENZhenqing, NIUHuawei
2014, 32(3): 388-394. DOI: 10.7638/kqdlxxb-2012.0130
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Application of DSMC method to study the impact diffusion characteristics of smoke particles
LIUGuosheng, GUANHua, SONGDongming, ZHANGQiqi
2014, 32(3): 395-399. DOI: 10.7638/kqdlxxb-2012.0132
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Aerodynamic design research on slat coves
DENGYiju, LIAOZhenrong, DUANZhuoyi
2014, 32(3): 400-404. DOI: 10.7638/kqdlxxb-2012.0137
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nvestigation of discharge coefficient with one inlet and double outlet hole injection
LIGuangchao, WUChaolin, ZHANGWei, ZHAOGuochang, KOUZhihai, LIUYu
2014, 32(3): 405-409. DOI: 10.7638/kqdlxxb-2012.0142
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Non-stationary analysis on field measured wind speed data of tall buildings
WUBengang, WUJiurong, FUJiyang
2014, 32(3): 410-415. DOI: 10.7638/kqdlxxb-2013.0027
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Wind tunnel test research of internal pressure response induced by oblique flow for rigid structure with opening
YUShice, LIQingxiang
2014, 32(3): 416-423. DOI: 10.7638/kqdlxxb-2013.0051
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