Effects of Fluid-Boundary Interaction on the Stability of Boundary Layers in Plasma Physics

Author(s):  
Masashi Ohnawa
2016 ◽  
Vol 35 (4) ◽  
pp. 1-8 ◽  
Author(s):  
Xinxin Zhang ◽  
Minchen Li ◽  
Robert Bridson

2013 ◽  
Vol 8 (4) ◽  
pp. 64-75
Author(s):  
Sergey Gaponov ◽  
Natalya Terekhova

This work continues the research on modeling of passive methods of management of flow regimes in the boundary layers of compressed gas. Authors consider the influence of pressure gradient on the evolution of perturbations of different nature. For low Mach number M = 2 increase in pressure contributes to an earlier transition of laminar to turbulent flow, and, on the contrary, drop in the pressure leads to a prolongation of the transition to turbulence. For high Mach number M = 5.35 found that the acoustic disturbances exhibit a very high dependence on the sign and magnitude of the external gradient, with a favorable gradient of the critical Reynolds number becomes smaller than the vortex disturbances, and at worst – boundary layer is destabilized directly on the leading edge


1997 ◽  
Author(s):  
Thorwald Herbert ◽  
Thorwald Herbert

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