TY - GEN
T1 - Application of the Time-Varying Koopman Operator for Bifurcation Analysis in Hypersonic erothermoelasticity
AU - Guého, Damien
AU - Huang, Daning
AU - Singla, Puneet
N1 - Funding Information:
This work is supported by the AFOSR grant FA9550-20-1-0176.
Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2022
Y1 - 2022
N2 - A time-varying Koopman operator (TVKO) is presented to study the nonlinear coupled dynamics between structural dynamics, heat transfer, and hypersonic aerothermodynamics, viz. AeroThermoElasticity (ATE). TVKO can be considered as an extension of the classical time-invariant Koopman operator (TIKO). It utilizes a subspace realization method known as the time-varying Eigensystem Realization Algorithm (TVERA) to approximate the underlying nonlinear model as a time varying linear model in a lifting space from time histories of inputoutput data. A benchmark model depicting the complex ATE dynamics for the flutter of a heated panel is considered to show the efficacy of the presented approach. The numerical experiments performed demonstrate the accuracy of the presented approach in capturing the bifurcation behavior in limit cycle oscillations due to variations in dynamic pressure.
AB - A time-varying Koopman operator (TVKO) is presented to study the nonlinear coupled dynamics between structural dynamics, heat transfer, and hypersonic aerothermodynamics, viz. AeroThermoElasticity (ATE). TVKO can be considered as an extension of the classical time-invariant Koopman operator (TIKO). It utilizes a subspace realization method known as the time-varying Eigensystem Realization Algorithm (TVERA) to approximate the underlying nonlinear model as a time varying linear model in a lifting space from time histories of inputoutput data. A benchmark model depicting the complex ATE dynamics for the flutter of a heated panel is considered to show the efficacy of the presented approach. The numerical experiments performed demonstrate the accuracy of the presented approach in capturing the bifurcation behavior in limit cycle oscillations due to variations in dynamic pressure.
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U2 - 10.2514/6.2022-0655
DO - 10.2514/6.2022-0655
M3 - Conference contribution
AN - SCOPUS:85123274582
SN - 9781624106316
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
BT - AIAA SciTech Forum 2022
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Y2 - 3 January 2022 through 7 January 2022
ER -