Excitation of the streaks by weak shock waves in the supersonic boundary layer
Abstract eng: The occurrence of the streaks was ... ... ... ... ... ... ... ... ... ... ... ... ... ... ... interaction of the weak shock waves with the flow in the vicinity of blunted leading edge. The process is accompanied by increasing of the local skin friction as well as the pulsation amplitude in the boundary layer. Here this simple case is discussed in comparison to the similar results obtained before in the boundary layer of the flat delta wing.
Publisher:
International Union of Theoretical and Applied Mechanics, 2016
Conference Title:
Conference Title:
24th International Congress of Theoretical and Applied Mechanics
Conference Venue:
Montreal (CA)
Conference Dates:
2016-08-21 / 2016-08-26
Rights:
Text je chráněný podle autorského zákona č. 121/2000 Sb.
Record appears in:
Record created 2016-11-15, last modified 2016-11-15
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