Rarefied hypersonic flow simulations using the Navier–Stokes equations with non-equilibrium boundary conditions-Reference-Cited by-同舟云学术

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Rarefied hypersonic flow simulations using the Navier–Stokes equations with non-equilibrium boundary conditions

Published:2012-07 Issue: Volume:52 Page:80-87
ISSN:0376-0421
Container-title:Progress in Aerospace Sciences
language:en
Short-container-title:Progress in Aerospace Sciences

Author:

Greenshields Christopher J.,Reese Jason M.

Funder

UK's Engineering and Physical Sciences Research Council

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference16 articles.

1. On stresses in rarefied gases arising from inequalities of temperature;Maxwell;Philosophical Transactions of the Royal Society of London,1879

2. Ueber wärmeleitung in verdünnten gasen;von Smoluchowski;Annalen der Physik und Chemie,1898

3. Velocity boundary condition at solid walls in rarefied gas calculations;Lockerby;Physical Review E,2004

4. Temperature jump and Knudsen layer in a rarefied gas over a plane wall: numerical analysis of the linearized Boltzmann equation for hard-sphere molecules;Sone;Physics of Fluids A,1989

5. Velocity slip and temperature jump coefficients for gaseous mixtures. I. Viscous slip coefficient;Sharipov;Physics of Fluids,2003

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