Copyright © A. Filippone (1996-2001). All Rights Reserved.
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Aerodynamic Drag

Wall Cooling



Wall cooling (in air) is used to damp the Tollmien- Schlichting waves, which increases the minimum critical Reynolds number for transition. The physical result is sketched in the figure below.


Figure 1: wall cooling effect on critical Reynolds number.

Skin friction drag reduction rates of up to 18 % have been measured in laboratory conditions on a flat plate. The cooling method is however unpractical in general cases (for ex. aviation), and might be confined to laboratory devices.



Copyright © A. Filippone (1996-2001). All Rights Reserved.