000013870 001__ 13870
000013870 005__ 20161115094004.0
000013870 04107 $$aeng
000013870 046__ $$k2016-08-21
000013870 100__ $$aLiu, Chao
000013870 24500 $$aStudy of heat-transfer coefficient on hypersonic boundary layer flow over a flat

000013870 24630 $$n24.$$p24th International Congress of Theoretical and Applied Mechanics - Book of Papers
000013870 260__ $$bInternational Union of Theoretical and Applied Mechanics, 2016
000013870 506__ $$arestricted
000013870 520__ $$2eng$$aMethod of computing convective heat transfer coefficient is examined by the numerical study on hypersonic boundary layer flow over a flat plate. For the similar solutions existing in hypersonic boundary layer flow for the variable specific heat, the heat flux on isothermal wall is calculated and being served as a standard to examine the accuracy of the method. The results showed that reference enthalpy method is more applicability than reference temperature method for variable specific heat. Then, using the formula above as the wall temperature condition, the DNS is conducted from an initially given temperature to adiabatic temperature for one meter long flat with incoming flow Mach number 4.5. According to the calculation results, we found that the temperature and heat flux on the wall associated with time and distance to the flat front edge.

000013870 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000013870 653__ $$a

000013870 7112_ $$a24th International Congress of Theoretical and Applied Mechanics$$cMontreal (CA)$$d2016-08-21 / 2016-08-26$$gICTAM2016
000013870 720__ $$aLiu, Chao
000013870 8560_ $$ffischerc@itam.cas.cz
000013870 8564_ $$s146668$$uhttps://invenio.itam.cas.cz/record/13870/files/PO.FM05-1.05.18.pdf$$yOriginal version of the author's contribution as presented on CD, XMLout( page 755, code PO.FM05-1.05.18).
000013870 962__ $$r13812
000013870 980__ $$aPAPER