000013839 001__ 13839
000013839 005__ 20161115094003.0
000013839 04107 $$aeng
000013839 046__ $$k2016-08-21
000013839 100__ $$aCui, Kai
000013839 24500 $$aStudy of shock wave/boundary layer interactions on high-pressure capturing wings

000013839 24630 $$n24.$$p24th International Congress of Theoretical and Applied Mechanics - Book of Papers
000013839 260__ $$bInternational Union of Theoretical and Applied Mechanics, 2016
000013839 506__ $$arestricted
000013839 520__ $$2eng$$aTo evaluate the heating load of high-pressure capturing wings (HCW) at various design conditions, a series of numerical cases were carried out to study the shock wave/boundary layer interactions between the inclined shock wave compressed by the airframe and the HCW. The results show that the maximal value of the heat-flux on the lower surface of the HCW decreases with the increase of the blunt radius of the HCW, the backward position of the inclined shock wave, and the decrease of the Reynolds number. While it increases with the increase of both the Mach number and the half cone angle. Besides, the maximal value of the heat-flux on the lower surface of the HCW is significantly lower than the value on the stagnation point. The present results show that the HCW configuration should have a good application prospect.

000013839 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000013839 653__ $$a

000013839 7112_ $$a24th International Congress of Theoretical and Applied Mechanics$$cMontreal (CA)$$d2016-08-21 / 2016-08-26$$gICTAM2016
000013839 720__ $$aCui, Kai
000013839 8560_ $$ffischerc@itam.cas.cz
000013839 8564_ $$s150824$$uhttps://invenio.itam.cas.cz/record/13839/files/PO.FM02-1.06.72.pdf$$yOriginal version of the author's contribution as presented on CD, XMLout( page 562, code PO.FM02-1.06.72).
000013839 962__ $$r13812
000013839 980__ $$aPAPER