Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
808589 | Theoretical and Applied Mechanics Letters | 2014 | 39988 Pages |
Abstract
The gap effect is a key factor in the design of the heat sealing in supersonic vehicles subjected to an aerodynamic heat load. Built on S-A turbulence model and Roe discrete format, the aerodynamic environment around a gap on the surface of a supersonic aircraft was simulated by the finite volume method. As the presented results indicate, the gap effect depends not only on the attack angle, but also on the Mach number.
Related Topics
Physical Sciences and Engineering
Engineering
Mechanical Engineering