Validation of a near-body and off-body grid partitioning methodology for aircraft aerodynamic performance prediction

DOI10.1016/J.COMPFLUID.2015.05.021zbMath1390.76257OpenAlexW367974852MaRDI QIDQ1645843

Stéphanie Péron, Ludovic Wiart, Pascal Raud, Christophe Benoit, Elie Gournay, Julien Mayeur, David Hue, Olivier Atinault

Publication date: 22 June 2018

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2015.05.021

zbMATH Keywords

dragaircraftmeshingCFDoversetCartesian

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Mesh generation, refinement, and adaptive methods for boundary value problems involving PDEs (65N50)

Uses Software

• Overture
• elsA
• OVERFLOW 2
• Spalart-Allmaras

Cites Work

• Parallel domain connectivity algorithm for unsteady flow computations using overlapping and adaptive grids
• Adaptive spatial partitioning and refinement for overset structured grids
• Drag/thrust analysis of jet-propelled transonic transport aircraft; Definition of physical drag components

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