CFD BASED COMPARISON OF FLUTTER EFFECT IN SUPERSONIC WING DESIGNS AT STEADY AERODYNAMIC CONDITION

• Author(s):

  Varunkumar K S | Nikhil N Gangamkote

• Keywords:

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

• 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

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Other Details

• Paper id:

  IJSARTV10I276499

• Published in:

  Volume: 10 Issue: 2 February 2024

• Publication Date:

  2024-02-05

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