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AAE 556 Aeroelasticity Lecture 24

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1 AAE 556 Aeroelasticity Lecture 24
Modal coordinates Purdue Aeroelasticity

2 Modal analysis objectives
Accurate flutter analysis with few degrees of freedom Identification of interaction in terms of physically meaningful motion – vibration mode shapes obtained from testing or analysis Key words Modal orthogonality generalized mass & stiffness Purdue Aeroelasticity

3 Reducing the number of system degrees of freedom
Vibration equations with quasi-steady loads This can be a really big eigenvalue problem with “n” degrees of freedom Let’s reduce the problem to “m” degrees of freedom and retain accuracy Purdue Aeroelasticity

4 Purdue Aeroelasticity
Begin with eigenvalue/eigenvector analysis for free vibration frequencies and mode shapes Solve for eigenvectors (mode shapes) construct a modal matrix from the eigenvectors Modal matrix Eigenvectors (mode shapes) Purdue Aeroelasticity

5 Purdue Aeroelasticity
Define response in terms of modal amplitude coordinates, h(t), and eigenvectors System response Modal matrix This series can be truncated to reduce DOF number from n to m (m<n) We go from n actual displacements (the x’s) to a m displacements (the h’s) Purdue Aeroelasticity

6 Example – String with tension S and three equal masses, m
Purdue Aeroelasticity

7 Purdue Aeroelasticity
Any general deflection can be constructed as a summation of normal modes Purdue Aeroelasticity

8 Use new (modal) coordinates to define motion
Purdue Aeroelasticity

9 Redefine motion in terms of modal coordinates
Pre- and post-multiply by the modal matrix Purdue Aeroelasticity

10 Purdue Aeroelasticity
Compute matrix products involving the mode shapes and the mass matrix The generalized masses and orthogonality Purdue Aeroelasticity

11 Generalized masses (in general) we diagonalize the mass matrix
Generalized mass matrix definition Diagonal matrix Purdue Aeroelasticity

12 Stiffness matrix multiplication
Purdue Aeroelasticity

13 Stiffness matrix multiplication showing orthogonality
Purdue Aeroelasticity

14 Final result with new coordinates a set of totally decoupled equations
Purdue Aeroelasticity

15 Purdue Aeroelasticity
One more step Purdue Aeroelasticity

16 Generalized stiffness matrix
Diagonal matrix Purdue Aeroelasticity

17 General aeroelastic system with aero displacement dependent loads
The matrix order can be reduced from n degrees of freedom to m degrees of freedom so that the matrix is smaller but still has a great deal of information content Purdue Aeroelasticity


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