Control-fluid interaction in air-conditioned aircraft cabins. A demonstration of stability analysis for partitioned dynamical systems.

DOI10.1016/S0045-7825(03)00427-4zbMath1054.76553OpenAlexW1505591565MaRDI QIDQ1421006

J. M. A. Hofman

Publication date: 23 January 2004

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/s0045-7825(03)00427-4

zbMATH Keywords

Gauss-Seidel schemeCoupled systemsAir-conditioningJacobi schemePartitioned analysisStaggered solution

Mathematics Subject Classification ID

Dynamical systems in control (37N35) Simulation of dynamical systems (37M05) Flow control and optimization for compressible fluids and gas dynamics (76N25) Numerical problems in dynamical systems (65P99)

Cites Work

• Two efficient staggered algorithms for the serial and parallel solution of three-dimensional nonlinear transient aeroelastic problems
• Partitioned procedures for the transient solution of coupled aeroelastic problems. I: Model problem, theory and two-dimensional application.
• New, quasi-simultaneous method to calculate interacting boundary layers
• Geometric multigrid with applications to computational fluid dynamics
• Partitioned procedures for the transient solution of coupled aeroelastic problems. II: Energy transfer analysis and three-dimensional applications
• Partitioned analysis of coupled mechanical systems
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