Investigation of aerodynamic characteristics of rarefied flow around NACA 0012 airfoil using DSMC and NS solvers

DOI10.1016/j.euromechflu.2014.04.008zbMath1408.76346OpenAlexW2036918074MaRDI QIDQ1670068

Peng Zhang

Publication date: 4 September 2018

Published in: European Journal of Mechanics. B. Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.euromechflu.2014.04.008

zbMATH Keywords

NACA 0012 airfoilOpenFOAMDSMCrarefied flowslip/jump boundary conditions

Mathematics Subject Classification ID

Rarefied gas flows, Boltzmann equation in fluid mechanics (76P05) General aerodynamics and subsonic flows (76G25)

Related Items (5)

DSMC simulation of hypersonic flows using an improved SBT-TAS technique ⋮ Evaluation of the SBT-TAS collision scheme on treating unsteady flows ⋮ A generalized form of the Bernoulli trial collision scheme in DSMC: derivation and evaluation ⋮ Evaluation of new collision-pair selection models in DSMC ⋮ The effects of gurney flap on the aerodynamic performance of NACA 0012 airfoil in the rarefied gas flow

Uses Software

• OpenFOAM
• dsmcFoam

Cites Work

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• Predicting failure of the continuum fluid equations in transitional hypersonic flows
• A hybrid DSMC/Navier–Stokes frame to solve mixed rarefied/nonrarefied hypersonic flows over nano‐plate and micro‐cylinder

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