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Volume 10, Issue 2 (February 2024)

Cfd Based Comparison Of Flutter Effect In Supersonic Wing Designs At Steady Aerodynamic Condition

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Volume 12 Issue 07

July 2026

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Author(s)

Varunkumar K S Nikhil N Gangamkote

Abstract

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 Of Stiffness. T


Keywords

Flutter Effect Aeroelasticity Steady Aerodynamics Computational Fluid Dynamics Supersonic Speed Conditions Fluid-Structure Interaction.

Paper ID

IJSARTV10I276499

Publication Date

February 5, 2024

Research Area

Mechanical Engineering

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