Numerical investigation of wall heat transfer influence on shock train in Scramjet isolator


Abstract eng:
Due 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].

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.



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 Record created 2016-11-15, last modified 2016-11-15


Original version of the author's contribution as presented on CD, XMLout( page 703, code PO.FM04-1.04.11).:
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