000014501 001__ 14501
000014501 005__ 20161115100153.0
000014501 04107 $$aeng
000014501 046__ $$k2016-08-21
000014501 100__ $$aKosinov, Alexander
000014501 24500 $$aExcitation of the streaks by weak shock waves in the supersonic boundary layer

000014501 24630 $$n24.$$p24th International Congress of Theoretical and Applied Mechanics - Book of Papers
000014501 260__ $$bInternational Union of Theoretical and Applied Mechanics, 2016
000014501 506__ $$arestricted
000014501 520__ $$2eng$$aThe 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.

000014501 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000014501 653__ $$a

000014501 7112_ $$a24th International Congress of Theoretical and Applied Mechanics$$cMontreal (CA)$$d2016-08-21 / 2016-08-26$$gICTAM2016
000014501 720__ $$aKosinov, Alexander
000014501 8560_ $$ffischerc@itam.cas.cz
000014501 8564_ $$s218534$$uhttps://invenio.itam.cas.cz/record/14501/files/TS.FM04-5.03.pdf$$yOriginal version of the author's contribution as presented on CD,  page 695, code TS.FM04-5.03
.
000014501 962__ $$r13812
000014501 980__ $$aPAPER