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AAE 556 Aeroelasticity Lecture 24
Modal coordinates Purdue Aeroelasticity
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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
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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
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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
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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
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Example – String with tension S and three equal masses, m
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Purdue Aeroelasticity
Any general deflection can be constructed as a summation of normal modes Purdue Aeroelasticity
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Use new (modal) coordinates to define motion
Purdue Aeroelasticity
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Redefine motion in terms of modal coordinates
Pre- and post-multiply by the modal matrix Purdue Aeroelasticity
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Purdue Aeroelasticity
Compute matrix products involving the mode shapes and the mass matrix The generalized masses and orthogonality Purdue Aeroelasticity
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Generalized masses (in general) we diagonalize the mass matrix
Generalized mass matrix definition Diagonal matrix Purdue Aeroelasticity
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Stiffness matrix multiplication
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Stiffness matrix multiplication showing orthogonality
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Final result with new coordinates a set of totally decoupled equations
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Purdue Aeroelasticity
One more step Purdue Aeroelasticity
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Generalized stiffness matrix
Diagonal matrix Purdue Aeroelasticity
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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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