TY - GEN
T1 - Modeling structural nonlinearities including damage using reduced order methods
AU - Rajadas, John
AU - Chattopadhyay, Aditi
AU - Munteanu, Sorin
PY - 2007
Y1 - 2007
N2 - A reduced order model (ROM) for addressing nonlinear aeroelasticity problem, including both structural and aerodynamic nonlinearities, has been developed. The CFD-based procedure captures the essence of an aerodynamic system while reducing its computational complexity. An Eigensystem Realization Algorithm is used to convert the ROM unsteady aerodynamics into the LTI state space model. A reduction in the cost of the realization of the ROM kernel is obtained by the identification of the state-space model. A micro-macro composite analysis that includes nonlinear strain rate effects and is capable of modeling in situ defects, such as cracks and delaminations, is used in the structural analysis of polymer matrix composite laminates. These nonlinearities are included in nonlinear time invariant structural ROMs which are identified for various cases of strain rates. Aeroelastic analysis is conducted using the nonlinear state space model. The state-space model is a highly optimized decoupled system while retaining significant details of the aeroelastic system. The approach used is computationally efficient and will be an essential element in damage detection and structural health monitoring (SHM) where multiple solutions of the "forward" problem is necessary in order to solve the inverse problem.
AB - A reduced order model (ROM) for addressing nonlinear aeroelasticity problem, including both structural and aerodynamic nonlinearities, has been developed. The CFD-based procedure captures the essence of an aerodynamic system while reducing its computational complexity. An Eigensystem Realization Algorithm is used to convert the ROM unsteady aerodynamics into the LTI state space model. A reduction in the cost of the realization of the ROM kernel is obtained by the identification of the state-space model. A micro-macro composite analysis that includes nonlinear strain rate effects and is capable of modeling in situ defects, such as cracks and delaminations, is used in the structural analysis of polymer matrix composite laminates. These nonlinearities are included in nonlinear time invariant structural ROMs which are identified for various cases of strain rates. Aeroelastic analysis is conducted using the nonlinear state space model. The state-space model is a highly optimized decoupled system while retaining significant details of the aeroelastic system. The approach used is computationally efficient and will be an essential element in damage detection and structural health monitoring (SHM) where multiple solutions of the "forward" problem is necessary in order to solve the inverse problem.
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M3 - Conference contribution
AN - SCOPUS:34547518897
SN - 1563478927
SN - 9781563478925
T3 - Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
SP - 7272
EP - 7289
BT - Collection of Technical Papers - 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
T2 - 48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Y2 - 23 April 2007 through 26 April 2007
ER -