Improvement of Airfoils Aerodynamic Efficiency by Thermal Camber Phenomenon at Low Reynolds Number

Improvement of Airfoils Aerodynamic Efficiency by Thermal Camber Phenomenon at Low Reynolds Number

In this research, viscous, laminar and steady flow around symmetric and non-symmetric airfoils is simulated at Low Reynolds Number (LRN). Navier-Stokes (N-S) equations are discretized by Finite Volume Method (FVM) and are solved by the SIMPLE algorithm in an open source software, namely OpenFOAM. Th...

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Bibliographic Details
Main Authors: Ahmad Samiee, Mohammad Hassan Djavareshkian, Behzad Forouzi Feshalami, Esmaeil Esmaeilifar
Format: Article
Language:English
Published: Instituto de Aeronáutica e Espaço (IAE) 2018-11-01
Series:Journal of Aerospace Technology and Management
Subjects:
Thermal camber
Aerodynamic
CFD
Low Reynolds number
Online Access:https://www.jatm.com.br/jatm/article/view/954

Internet

https://www.jatm.com.br/jatm/article/view/954

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