HYBRID GRID APPROACH TO STUDY DYNAMIC STALL

被引：4
|
作者：
REU, T
YING, SX
机构：
[1] FLORIDA STATE UNIV,DEPT MECH ENGN,FAMU,TALLAHASSEE,FL 32306
[2] FLORIDA STATE UNIV,SUPERCOMP COMPUTAT RES INST,TALLAHASSEE,FL 32306
来源：
AIAA JOURNAL | 1992年 / 30卷 / 11期
关键词：
D O I：
10.2514/3.11283
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A hybrid structured and unstructured grid scheme is developed to study dynamic stall over an airfoil in a wind tunnel. The unsteady Navier-Stokes equations are solved implicitly using this hybrid grid scheme. Results are compared with experimental data. Additionally, they reveal informative details of the flowfield physics associated with dynamic stall.
引用
收藏
页码：2670 / 2676
页数：7
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