CONTENTS l Introduction l Mode Superposition Method for
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CONTENTS l Introduction l Mode Superposition Method for Classically Damped Systems l Mode Superposition Method for Non-Classically Damped Systems l Numerical Examples l Conclusions Structural Dynamics & Vibration Control Lab. , KAIST 2
INTRODUCTION Background l Dynamic Equations of Motion (1) where M C K u(t) f(t) : : : Mass matrix of order n Damping matrix of order n Stiffness matrix of order n Displacement vector Load vector l Methods of Dynamic Analysis w Direct integration method w Mode superposition method Structural Dynamics & Vibration Control Lab. , KAIST 3
l Advantages of Mode Superposition Method w Effective because of using a few modes w Gives the dynamic characteristics of each mode w Effective for long duration loading l Drawbacks of Mode Superposition Method w Fail to give an accurate solution w Need to consider the effects of truncated high modes l Improved Mode Superposition Methods w Mode acceleration method (MA method) w Modal truncation augmentation method (MT method) Structural Dynamics & Vibration Control Lab. , KAIST 4
Non-classically Damped System l Decoupling the System (1) (2) where l If Cg has off-diagonal elements, C is called as non-classical damping approximate to classically damped system so, off-diagonal terms are ignored Structural Dynamics & Vibration Control Lab. , KAIST 5
Objective In this study, improved mode superposition methods are applied to non-classically damped system Structural Dynamics & Vibration Control Lab. , KAIST 6
MODE SUPERPOSISTION METHOD FOR CLASSICALLY DAMPED SYSTEM Mode Superposition Method l The Dynamic Equations of Motion (1) l Decoupled Equations by Eigenvectors (2) l Displacements us(t) (3) where Structural Dynamics & Vibration Control Lab. , KAIST 7
Mode Acceleration Method (MA Method) l The Solution by MA Method (4) (5) (6) where us(t) : displacements modally represented ut(t) : displacements not represented by the modes r(t) : time varying portion of f(t) R 0 : invariant spatial portion of f(t) Structural Dynamics & Vibration Control Lab. , KAIST 8
l The Portion of MA Solution w us(t) : displacements modally represented (7) w ut(t) : displacements not represented by the modes (8) where : force truncation vector : modally represented spatial load vector MA method approximates ut(t) by a static solution Structural Dynamics & Vibration Control Lab. , KAIST 9
Modal Truncation Augmentation Method (MT Method) l The Solution by MT Method (4) l The Portion of Solution w us(t) : displacements modally represented (7) w ut(t) : displacements not represented by the modes (9) MT method approximates ut(t) by a dynamic solution Structural Dynamics & Vibration Control Lab. , KAIST 10
l Derivation of Pseudo Eigenvector P (10) where Structural Dynamics & Vibration Control Lab. , KAIST 11
MODE SUPERPOSISTION METHOD FOR NON-CLASSICALLY DAMPED SYSTEM State Space Equations l State Space Equations (11) where Structural Dynamics & Vibration Control Lab. , KAIST 12
l Associated Eigenvalue Problem (12) l Eigenvalue and Eignevector (13) where Structural Dynamics & Vibration Control Lab. , KAIST 13
l Mode Superposition Method in Non-Classically Damped System w State space equation (11) w Decouple the eqn. (3) by complex eigenvector (14) w Displacements ys(t) (15) Eigenvectors are conjugate pairs (16) Structural Dynamics & Vibration Control Lab. , KAIST 14
MA Method l The Solution by MA Method (17) (18) where ys(t) : displacements modally represented yt(t) : displacements not represented by the modes r(t) : time varying portion of F(t) R 0 : invariant spatial portion of F(t) Structural Dynamics & Vibration Control Lab. , KAIST 15
l The Portion of Solution w ys(t) : displacements modally represented (19) w yt(t) : displacements not represented by the modes (20) where : force truncation vector : modally represented spatial load vector y(t) is calculated from conjugate pair MA method approximates yt(t) by a static solution Structural Dynamics & Vibration Control Lab. , KAIST 16
MT Method l The Solution by MT Method (17) l The Portion of Solution w ys(t) : displacements modally represented (19) w yt(t) : displacements not represented by the modes (21) MT method approximates yt(t) by a dynamic solution Structural Dynamics & Vibration Control Lab. , KAIST 17
l Derivation of Pseudo Eigenvector P (22) where Structural Dynamics & Vibration Control Lab. , KAIST 18
NUMERICAL EXAMPLES l Structures w Four-story shear building w Cantilever beam with multi-lumped dampers l Comparisons w Displacement responses w Displacement error of each method Structural Dynamics & Vibration Control Lab. , KAIST 19
Four-Story Shear Building R 0 cos t M 1 K 2 K 3 K 4 M 2 M 3 M 4 U 1 U 2 U 3 • Input load ( R 0 cos. Wt ) R 0=1 W = 7 rad/sec (≒ 0. 5 w 1 ) w 1 = - 0. 0317 ± 13. 2935 i w 2 = - 0. 0007 ± 29. 6597 i U 4 Structural Dynamics & Vibration Control Lab. , KAIST 20
Displacement Responses (using 1 mode) Time(sec) Structural Dynamics & Vibration Control Lab. , KAIST 21
Displacement Responses(using 2 modes) Time(sec) Structural Dynamics & Vibration Control Lab. , KAIST 22
Displacement Error Using 2 Modes Difference Using 1 Mode Time(sec) Structural Dynamics & Vibration Control Lab. , KAIST 23
Cantilever beam with multi-lumped dampers R 0 sin(W t) 1 2 3 45 14 • Material property Tangential damper, c : 0. 3 Young’s modulus : 100 Mass density : 1 Moment of inertia : 1 Cross-section area : 1 • Input 49 50 load ( R 0 cos. Wt ) R 0=1 W = 5 rad/sec (≒ 0. 6 w 1 ) w 1 = -0. 2696877077± 7. 7304416035 i w 2 = -0. 4278691331± 9. 7835115896 i Structural Dynamics & Vibration Control Lab. , KAIST 24
Displacement Responses (using 1 mode) Time(sec) Structural Dynamics & Vibration Control Lab. , KAIST 25
Displacement Responses (using 2 modes) Time(sec) Structural Dynamics & Vibration Control Lab. , KAIST 26
Displacement Error Using 1 Mode Time(sec) Using 2 Modes Time(sec) Structural Dynamics & Vibration Control Lab. , KAIST 27
CONCLUSIONS u Improved mode superposition methods are applied to non-classically damped systems. u MA method and MT method are more efficient than simple mode superposition method. u MA method and MT method have same convergence rate in non-classically damped system. Structural Dynamics & Vibration Control Lab. , KAIST 28
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