column
Display Method:
Method for evaluating spatial accuracy order of CFD and applications to WCNS scheme on four typically distorted meshes
TU Guohua, DENG Xiaogang, MIN Yaobing, MAO Meiliang, LIU Huayong
2014, 32(4): 425-432. DOI: 10.7638/kqdlxxb-2012.0192
Abstract PDF
Interference effects of wing-mounted high bypass ratio nacelle with engine power
QIAO Lei, BAI Junqiang, HUA Jun, CHEN Yingchun, ZHANG Miao, ZHANG Meihong
2014, 32(4): 433-438. DOI: 10.7638/kqdlxxb-2012.0196
Abstract PDF
Numerical simulation of high lift trapezoidal wing configuration with WCNS-E-5 scheme
LI Song, WANG Guangxue, WANG Yuntao, ZHANG Yulun, DENG Xiaogang
2014, 32(4): 439-445. DOI: 10.7638/kqdlxxb-2012.0188
Abstract PDF
Analysis of propulsive performance for dual flapping airfoils using CFD method
ZHANG Weiwei, XU Yang, JIANG Yuewen, YE Zhengyin
2014, 32(4): 446-452. DOI: 10.7638/kqdlxxb-2012.0148
Abstract PDF
A study of gridless method based on third┈order WENO reconstruction
PU Saihu, CHEN Hongquan
2014, 32(4): 453-461. DOI: 10.7638/kqdlxxb┈2012.0149
Abstract PDF
An original designed limiter for discontinuous Galerkin method
GUO Yongheng, YANG Yong, LIU Yiou
2014, 32(4): 462-467. DOI: 10.7638/kqdlxxb-2012.0157
Abstract PDF
Dynamic mesh based wing design optimization of HALE aircraft
ZHU Xiongfeng, GUO Zheng, HOU Zhongxi
2014, 32(4): 468-474. DOI: 10.7638/kqdlxxb-2012.0144
Abstract PDF
Concept and experimental validation of adaptive pressure relief control for fixed geometry hypersonic inlets
JIN Zhiguang, ZHANG Kunyuan, LIU Yuan
2014, 32(4): 475-480. DOI: 10.7638/kqdlxxb-2012.0145
Abstract PDF
A numerical approach for fast simulation of unsteady flow around oscillating cascades
SHI Yongqiang, YANG Qingzhen, HUANG Xiuquan, GUO Xiao
2014, 32(4): 481-487. DOI: 10.7638/kqdlxxb-2012.0146
Abstract PDF
Investigation about transonic wind tunnel test section noise mechanism based on experimental
LU Jinlei, SHENG Meiping, LIAO Daxiong, WANG Haifeng
2014, 32(4): 488-492. DOI: 10.7638/kqdlxxb-2012.0151
Abstract PDF
Aerodynamics configuration study for CSTS reentry capsule
YANG Xiaofeng, TANG Wei, GUI Yewei
2014, 32(4): 493-498. DOI: 10.7638/kqdlxxb-2012.0154
Abstract PDF
The research of aerodynamic characteristics of high-lift configuration of large transport plane with the effect of engine jet
BAI Junqiang, ZHANG Xiaoliang, LIU Nan, DONG Jianhong, DONG Qiang, ZHOU Lin
2014, 32(4): 499-505. DOI: 10.7638/kqdlxxb-2012.0158
Abstract PDF
A virtual sub-cells technique with transient adaptive collision distance for the DSMC method
HUANG Fei, CHEN Zhi, CHENG Xiaoli, SHEN Qing
2014, 32(4): 506-510. DOI: 10.7638/kqdlxxb-2012.0161
Abstract PDF
Influence of the molecule number on nitrogen-oxygen dissociation reacting flows in DSMC simulations
YANG Haosen, ZHANG Bin, LIU Hong, CHEN Fang
2014, 32(4): 511-517. DOI: 10.7638/kqdlxxb-2012.0164
Abstract PDF
Kriging-based airfoil inverse design
LIU Jun, SONG Wenping, HAN Zhonghua, XU Jianhua, FAN Yanhong
2014, 32(4): 518-526. DOI: 10.7638/kqdlxxb-2012.0165
Abstract PDF
Computational research on aerodynamic forces of scissors tail-rotor in forward flight based on the N-S equations
FAN Feng, XU Guohua, SHI Yongjie
2014, 32(4): 527-533. DOI: 10.7638/kqdlxxb-2012.0166
Abstract PDF
Large-eddy simulation of fully developed turbulent flow over a wavy surface
SUN Liming, CAO Shuyang, LI Ming, YANG Qing, ZHANG Enzhen
2014, 32(4): 534-543. DOI: 10.7638/kqdlxxb-2012.0172
Abstract PDF
Experimental and theoretical analysis of water exit of a supercavity
SHI Honghui, HU Junhui, ZHOU Haolei
2014, 32(4): 544-550. DOI: 10.7638/kqdlxxb-2013.0008
Abstract PDF
An automatic differentiation method for uncertainty analysis due to airfoil configuration variation
XU Lincheng, WANG Gang, WU Jie, YE Zhengyin
2014, 32(4): 551-556. DOI: 10.7638/kqdlxxb-2013.0097
Abstract PDF