STABILIZATION OF A HYPERSONIC BOUNDARY LAYER USING PASSIVE POROUS COATINGS |
| 4 | |
| 2011 |
| scientific article | 532.526.3 | ||
| 2615-2616 |
| Experimental results of investigating the effect of the thickness of a passive porous coating on the development of natural disturbances in a hypersonic boundary layer, using the model of a sharp cone for the zero angle of attack and Mach number of M = 6, are presented. An optimal thickness of the porous coating providing the maximum stabilization effect of second mode disturbances is shown to exist. |
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