Comparison between Mach 2 rarefied airflow modification by an electrical discharge and numerical simulation of airflow modification by surface heating

DOI10.1063/1.3234365zbMath1183.76406OpenAlexW2066097483MaRDI QIDQ5304865

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Publication date: 18 March 2010

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

Full work available at URL: https://doi.org/10.1063/1.3234365

zbMATH Keywords

shock wavesboundary layersMach numberflow simulationnumerical analysiselectrodesrarefied fluid dynamicsdischarges (electric)

Mathematics Subject Classification ID

Fluid mechanics (76-XX)

Cites Work

• Unnamed Item
• Comparison of kinetic and continuum approaches for simulation of shock wave/boundary layer interaction
• Application of the Cercignani-Lampis scattering kernel to calculations of rarefied gas flows. II: Slip and jump coefficients.
• Navier-Stokes computations in micro shock tubes
• Flow Control

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