Derivation of the viscous Moore-Greitzer equation for aeroengine flow

DOI10.1063/1.2534332zbMath1144.81315OpenAlexW2116667053MaRDI QIDQ3529770

Songming Hou, Niklas Wellander, Björn Birnir

Publication date: 14 October 2008

Published in: Journal of Mathematical Physics (Search for Journal in Brave)

Full work available at URL: https://escholarship.org/uc/item/8sk0b2q4

zbMATH Keywords

modelinghomogenizationscalingtwo-scale convergencecompressorjet engine flowSeparation of scales

Mathematics Subject Classification ID

Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (4)

Hopf bifurcations of Moore-Greitzer PDE model with additive noise ⋮ Asymptotic analysis and error estimates for an optimal control problem with oscillating boundaries ⋮ Stokes’ System in a Domain with Oscillating Boundary: Homogenization and Error Analysis of an Interior Optimal Control Problem ⋮ Exact internal controllability for the wave equation in a domain with oscillating boundary with Neumann boundary condition

Cites Work

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• An explicit description of the global attractor of the damped and driven sine-Gordon equation
• Inertial manifolds and Gevrey regularity for the Moore-Greitzer model of an axial-flow compressor
• Bifurcation Analysis of Axial Flow Compressor Stability
• A Finite Dimensional Attractor of the Moore--Greitzer PDE Model
• Center Manifold of the Viscous Moore--Greitzer PDE Model
• Basic Control for the Viscous Moore--Greitzer Partial Differential Equation
• Turbulent Combustion
• A Backstepping Controller for a Nonlinear Partial Differential Equation Model of Compression System Instabilities
• Dynamics and control of entrained solutions in multi-mode MooreGreitzer compressor models

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