LIMIT CYCLE OSCILLATION PREDICTION AND CONTROL DESIGN METHOD FOR AEROELASTIC SYSTEM BASED ON NEW NONLINEAR REDUCED ORDER MODEL

DOI10.1142/S0219876211002435zbMath1270.76068OpenAlexW2021405454MaRDI QIDQ2845373

Guirong Yan, Gang Chen, Yue-ming Li

Publication date: 30 August 2013

Published in: International Journal of Computational Methods (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1142/s0219876211002435

zbMATH Keywords

limit cycle oscillationactive controlproper orthogonal decompositionaeroelasticityreduced-order model

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Transonic flows (76H05) Finite volume methods applied to problems in fluid mechanics (76M12) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Related Items (3)

REDUCED-ORDER-MODEL-BASED PLACEMENT OPTIMIZATION OF MULTIPLE CONTROL SURFACES FOR ACTIVE AEROELASTIC CONTROL ⋮ Support-vector-machine-based reduced-order model for limit cycle oscillation prediction of nonlinear aeroelastic system ⋮ Reduced-Order Modeling Based on Hybrid Snapshot Simulation

Cites Work

• Reduced-order fluid/structure modeling of a complete aircraft configuration

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