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Volume 12 Issue 07
July 2026
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Author(s)
Chinmay Srinivas C Maruthi Kumar Giridhar Shingri Karthik C Veerapur, Madhu B. P
Abstract
In This Work ,NACA 0006 Aerofoil Was Analysed. The Analysis Carried Out Was By Varying Wind Velocities And Angles Of Attack Of NACA 0006 Aerofoil Model. Analysis Is Performed Experimentally In The Wind Tunnel Testing Facility And Similarly CFD Analysis
Keywords
Coefficient Of Drag
Coefficient Of Lift
Computational Fluid Dynamics
NACA 0006
NACA 0012
Paper ID
IJSARTV4I523392
Publication Date
May 8, 2018
Research Area
Mechanical Engineering