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A boundary element method for the aerodynamic analysis of aircraft in arbitrary motions

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Publication:1419909
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DOI10.1007/s00466-003-0487-3zbMath1038.76533OpenAlexW2012606865MaRDI QIDQ1419909

M. Gennaretti, Luigi Morino, Giovanni Bernardini

Publication date: 28 January 2004

Published in: Computational Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/s00466-003-0487-3


zbMATH Keywords

Boundary elementsRotor aerodynamics


Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) General theory of rotating fluids (76U05) Boundary element methods applied to problems in fluid mechanics (76M15)


Related Items (3)

Eigenanalysis and reduced-order modelling of unsteady partial cavity flows using the boundary element method ⋮ Continuous-time state-space unsteady aerodynamic modeling based on boundary element method ⋮ A new velocity decomposition for viscous flows: Lighthill's equivalent-source method revisited




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