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Aeroelasticity

Aeroelasticity. Instructor: Prof. C. Venkatesan, Department of Aerospace Engineering, IIT Kanpur. Aeroelasticity studies the interactions between the inertial, elastic, and aerodynamic forces that occur when an elastic body is exposed to a fluid flow. Topics covered in this course include: Aeroelastic problems; Deformation of structures and influence coefficients; Energy method; Classification and solution of aeroelastic problems; Static aeroelasticity; Dynamic aeroelasticity; Unsteady aeroelasticity; Flutter analysis of a wing. (from nptel.ac.in)

Lecture 04 - Energy Method (cont.)

Go to the Course Home or watch other lectures:

Lecture 01 - Introduction

Lecture 02 - Deformation of Structures and Influence Coefficients

Lecture 03 - How Energy Method is Applied for Getting the Deformations

Lecture 04 - Energy Method (cont.)

Lecture 05 - Application of Hamilton's Principle

Lecture 06 - Beam Bending Vibration Problem: Boundary Conditions

Lecture 07 - Solving Beam Bending Vibration Problems with Boundary Conditions

Lecture 08 - Classification and Solution of Aeroelastic Problems

Lecture 09 - Static Aeroelasticity

Lecture 10 - Torsional Deformation Equation of a Straight Wing

Lecture 11 - Wing Loading and Deformations

Lecture 12 - Swept Wing

Lecture 13 - Formulation for the Swept Wings, Divergence of 2D Airfoil and Straight Wing

Lecture 14 - Dynamic Aeroelasticity

Lecture 15 - Unsteady Aerodynamics: Continuity Equation

Lecture 16 - Unsteady Aerodynamics: Momentum Equation

Lecture 17 - Unsteady Aerodynamics (cont.)

Lecture 18 - Thin Aerofoil in Steady Supersonic Flow, Unsteady 2D Supersonic Flow

Lecture 19 - Unsteady 2D Supersonic Flow (cont.)

Lecture 20 - Subsonic Flow (Kernel Function Approach)

Lecture 21 - Two Dimensional Incompressible Flow

Lecture 22 - 2D Unsteady Incompressible Flow: Theodorsen Theory

Lecture 23 - Theodorsen Theory (cont.)

Lecture 24 - Dynamic Aeroelasticity: Flutter Problem

Lecture 25 - Unsteady Aerodynamic Models: Finite State Models

Lecture 26 - Flutter Analysis of a Wing of a Large Aspect Ratio Wing