000013865 001__ 13865
000013865 005__ 20161115094003.0
000013865 04107 $$aeng
000013865 046__ $$k2016-08-21
000013865 100__ $$aLu, Hongbo
000013865 24500 $$aNumerical investigation of wall heat transfer influence on shock train in Scramjet isolator

000013865 24630 $$n24.$$p24th International Congress of Theoretical and Applied Mechanics - Book of Papers
000013865 260__ $$bInternational Union of Theoretical and Applied Mechanics, 2016
000013865 506__ $$arestricted
000013865 520__ $$2eng$$aDue to the scramjet isolator suffering from the severe aeroheating problem at a long time fly, this paper studied the influence of wall heat transfer on flow characteristics and performance of a scramjet isolator by numerical simulation. The results show that shock train is affected by the dual mechanism of isolator wall temperature and airflow total temperature. Shock train length increases with ratio of wall temperature to total temperature. To predict shock train length of practical design with more accuracy, the parameter involved wall heat transfer is introduced to improve Waltrup and Billig correlation [1].

000013865 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000013865 653__ $$a

000013865 7112_ $$a24th International Congress of Theoretical and Applied Mechanics$$cMontreal (CA)$$d2016-08-21 / 2016-08-26$$gICTAM2016
000013865 720__ $$aLu, Hongbo
000013865 8560_ $$ffischerc@itam.cas.cz
000013865 8564_ $$s168205$$uhttps://invenio.itam.cas.cz/record/13865/files/PO.FM04-1.04.11.pdf$$yOriginal version of the author's contribution as presented on CD, XMLout( page 703, code PO.FM04-1.04.11).
000013865 962__ $$r13812
000013865 980__ $$aPAPER