Investigation Of Cavity Designs On Various Airfoils
Aerodynamic efficiency loss in airfoils is primarily due to the increased drag caused by boundary layer separation, especially at low Reynolds number. To reenergise the boundary layer and delay flow separation, cavities are introduced on the suction side of the airfoil. A cavity is a passive flow...
Main Author: | Vasudevan, Yuvneesh |
---|---|
Format: | Monograph |
Language: | English |
Published: |
Universiti Sains Malaysia
2021
|
Subjects: | |
Online Access: | http://eprints.usm.my/54732/1/Investigation%20Of%20Cavity%20Designs%20On%20Various%20Airfoils.pdf |
Similar Items
-
Airfoil With Membrane At Low Reynolds Number
by: Roslan, Abdul Qayyum
Published: (2019) -
Aerodynamic Characteristics Of Membrane Airfoil Compared To Rigid Naca 4412 Airfoil
by: Chan, Min Xhao
Published: (2018) -
Numerical simulation of turbulent flow around an airfoil with blunt trailing edge aerodynamic characteristics modification of this airfoil with base and aerodynamic cavity
by: H Sayadi, et al.
Published: (2013-03-01) -
Aerodynamics Study Of Tubercle Effect On NACA4412 Airfoil
by: Enso, Ennelyn Novema
Published: (2017) -
Airfoil design and data /
by: 196368 Eppler, Richard
Published: (1990)