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Volume 12 Issue 07
July 2026
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Author(s)
Santhosh Kumar. J Omprakash. D Nataraj. R Shriram. P, Sridharan. M
Abstract
This Research Provides A Stable, High-efficiency, High Angle Of Attack, Airfoil. The Means Of Accomplishing These Improvements Is Based On The Concepts Of KF Airfoils. A Primary Objective Of This Research Is To Improve The Efficiency Of The Airfoil An
Keywords
Angle Of Attack
CFD Analysis
NACA 4415
NACA 0015
KF Airfoil
Lift
Drag
Paper ID
IJSARTV2I31978
Publication Date
March 26, 2016
Research Area
Aerodynamics