The effects of gurney flap on the aerodynamic performance of NACA 0012 airfoil in the rarefied gas flow

DOI10.1016/J.COMPFLUID.2018.05.003zbMath1410.76138OpenAlexW2801142557MaRDI QIDQ720902

E. Izadpanah, M. Liravi, Yasser Amini

Publication date: 18 July 2018

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

Full work available at URL: https://doi.org/10.1016/j.compfluid.2018.05.003

zbMATH Keywords

rarefied gasDSMCGurney flapMaxwell slip boundary conditionSmoluchowski jump boundary condition

Mathematics Subject Classification ID

Rarefied gas flows, Boltzmann equation in fluid mechanics (76P05) Hypersonic flows (76K05)

Uses Software

• pdFOAM

Cites Work

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• Assessment of the LD-DSMC hybrid method for hypersonic rarefied flow
• Investigation of aerodynamic characteristics of rarefied flow around NACA 0012 airfoil using DSMC and NS solvers
• New high-resolution central schemes for nonlinear conservation laws and convection-diffusion equations
• Semidiscrete Central-Upwind Schemes for Hyperbolic Conservation Laws and Hamilton--Jacobi Equations
• Velocity profile in the Knudsen layer according to the Boltzmann equation
• Implementation of semi-discrete, non-staggered central schemes in a colocated, polyhedral, finite volume framework, for high-speed viscous flows

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