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Vol 10, Issue 2 (February 2024)
Mechanical Engineering
CFD BASED COMPARISON OF FLUTTER EFFECT IN SUPERSONIC WING DESIGNS AT STEADY AERODYNAMIC CONDITION
This Research Paper Presents A Numerical Methodology And Analysis To Study The Aeroelastic Effect Of Flutter, Which Is A Self-exciting Oscillation That Can Occur On Wings At High Speeds; Particularly Referred To As The Twist Along Its Axis...
Flutter Effect
Aeroelasticity
Steady Aerodynamics
Computational Fluid Dynamics
Supersonic Speed Conditions
Varunkumar K S, Nikhil N Gangamkote