欢迎您!
东篱公司
退出
申报数据库
申报指南
立项数据库
成果数据库
期刊论文
会议论文
著 作
专 利
项目获奖数据库
位置:
成果数据库
>
期刊
> 期刊详情页
Aerodynamic airfoil design using the Euler equations based on the dynamic evolution method and the c
ISSN号:1674-7348
期刊名称:Science China Physics,Mechanics & Astonomy
时间:2011
页码:697-702
相关项目:快速畸变湍流的模式理论、数值模拟与实验研究
作者:
Gao Yingying|He Feng|Shen Mengyu|
同期刊论文项目
快速畸变湍流的模式理论、数值模拟与实验研究
期刊论文 30
同项目期刊论文
基于特征理论的二维无粘Lagrange流体力学有限体积法
Direct numerical simulation of a spatially developing compressible plane mixing layer: flow structur
Wing tip vortex structure behind an airfoil with flaps at the tip
Low dispersion finite volume scheme based on reconstruction with minimized dispersion and controllab
The multi-dimensional limiters for solving hyperbolic conservation laws on unstructured grids
he multi-dimensional limiters for solving hyperbolic conservation laws on unstructured grids II: Ext
High-resolution finite difference schemes using curvilinear coordinate grids for DNS of compressible
A class of finite difference schemes with low dispersion and controllable dissipation for DNS of com
Study of flow induced by sine wave and saw tooth plasma actuators
RANS modeling of high-speed aerodynamic flow transition with consideration of stability theory
Numerical investigation of the casing treatment mechanism with a single circumferential groove
Intermittent gas resonance in stage separation flow field of multistage rocket
Study of control effects of vortex generators on a supercritical wing
Analysis of the secondary instability of the incompressible flows over a swept wing
Secondary instability control of compressible flow by suction for a swept wing
Simulation of shock wave buffet and its suppression on an OAT15A supercritical airfoil by IDDES
Numerical Dissipation Effects on the Massive Separation around Tandem Cylinders
Numerical Investigation of Massively Separated Flows past Rudimentary Landing Gear Using Advanced DE
NSGA-Ⅱ算法的改进及其在多段翼型缝道参数优化中的应用
导弹大迎角下非线性诱导滚转力矩数值研究
Drag reduction of compressible wall turbulence with active dimples
短舱扰流片对运输机增升装置气动特性的影响
非定常动态演化伴随优化设计方法
组合小翼和翼梢喷流对翼尖涡的影响实验研究
Analysis of the dominant frequency in a subsonic compressor stator at near stall condition
可压缩横流失稳及其控制
翼梢小翼若干几何参数对翼尖涡流场的影响研究