000014493 001__ 14493
000014493 005__ 20161115100153.0
000014493 04107 $$aeng
000014493 046__ $$k2016-08-21
000014493 100__ $$aGrogan, Kevin
000014493 24500 $$aDetailed simulations of shock boundary layer interaction in shock tube experiments

000014493 24630 $$n24.$$p24th International Congress of Theoretical and Applied Mechanics - Book of Papers
000014493 260__ $$bInternational Union of Theoretical and Applied Mechanics, 2016
000014493 506__ $$arestricted
000014493 520__ $$2eng$$aDetailed simulations of inert, multi-dimensional, viscous, shock tube experiments are undertaken. From these simulations, distinct regimes of shock boundary layer interaction are observed. These regimes show a dependence on the composition of the test gas and the Mach number of the incident shock wave. From these simulations, it is suggested that tailoring the incident shock Mach number could reduce the inhomogeneity in the flow and increase the operable range in chemical kinetic experiments.

000014493 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000014493 653__ $$a

000014493 7112_ $$a24th International Congress of Theoretical and Applied Mechanics$$cMontreal (CA)$$d2016-08-21 / 2016-08-26$$gICTAM2016
000014493 720__ $$aGrogan, Kevin
000014493 8560_ $$ffischerc@itam.cas.cz
000014493 8564_ $$s165887$$uhttps://invenio.itam.cas.cz/record/14493/files/TS.FM04-3.05.pdf$$yOriginal version of the author's contribution as presented on CD,  page 679, code TS.FM04-3.05
.
000014493 962__ $$r13812
000014493 980__ $$aPAPER