Using Adaptive Meshing for Solving the Transonic Flow around Airfoils
Numerical analyses have shown that successful flow simulations and the accuracy of solution noticeably depend on the number of nodes used in computational meshing. A suitable meshing should have the capability of adapting with main flow parameters. Because the number of total nodes that can be used...
Main Authors: | Sayed AmirAbbas Oloumi, Mehran Ameri |
---|---|
Format: | Article |
Language: | English |
Published: |
Islamic Azad University-Isfahan (Khorasgan) Branch
2008-06-01
|
Series: | International Journal of Advanced Design and Manufacturing Technology |
Online Access: | https://admt.isfahan.iau.ir/article_534665_fd19464ff65c601576f24020ebc363f9.pdf |
Similar Items
-
Transonic Airfoil Flow Simulation. Part I: Mesh Generation and Inviscid Method
by: Vladimir CARDOS, et al.
Published: (2010-06-01) -
ANALYSIS OF TRANSONIC FLOW PAST CUSPED AIRFOILS
by: Jiří Stodůlka, et al.
Published: (2015-06-01) -
Numerical Simulations on Unsteady Nonlinear Transonic Airfoil Flow
by: Diliana Friedewald
Published: (2020-12-01) -
Design of a transonic airfoil
by: Lim, Jing Kai.
Published: (2011) -
Flow Control of Transonic Airfoils using Optimum Suction and Injection Parameters
by: Zahra Seifollahi Moghadam, et al.
Published: (2017-01-01)