Abstract
In hypersonic aerodynamics and microflow device design, the momentum and energy fluxes to solid surfaces are often of critical importance. However, these depend on the characteristics of the Knudsen layer - the region of local non-equilibrium existing up to one or two molecular mean free paths from the wall in any gas flow near a surface. While the Knudsen layer has been investigated extensively using kinetic theory, the ability to capture it within a continuum-fluid formulation (in conjunction with slip boundary conditions) suitable for current computational fluid dynamics toolboxes would offer distinct and practical computational advantages.
Original language | English |
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Pages (from-to) | 1391-1393 |
Number of pages | 2 |
Journal | AIAA Journal |
Volume | 43 |
Issue number | 6 |
Publication status | Published - Jun 2005 |
Keywords
- knudsen layer
- gases
- atomic physics
- mechanical engineering
- hypersonic aerodynamics
- microflow devices