000014487 001__ 14487
000014487 005__ 20161115100153.0
000014487 04107 $$aeng
000014487 046__ $$k2016-08-21
000014487 100__ $$aPaolucci, Samuel
000014487 24500 $$aShock structure in hypersonic flows

000014487 24630 $$n24.$$p24th International Congress of Theoretical and Applied Mechanics - Book of Papers
000014487 260__ $$bInternational Union of Theoretical and Applied Mechanics, 2016
000014487 506__ $$arestricted
000014487 520__ $$2eng$$aThe structure of a gas-dynamic shock wave at hypersonic conditions is of great interest. The Navier–Stokes–Fourier formulation is known to yield incorrect shock profiles even at moderate Mach numbers. This is an excellent test problem for extensions of such equations for flows with large gradients since accurate experimental results are available. We present a second order formulation of the constitutive equations based solely on continuum theory. Results of the second-order theory applied to the shock structure are obtained for monatomic and diatomic gases over a large range of Mach numbers and are compared to experimental results.

000014487 540__ $$aText je chráněný podle autorského zákona č. 121/2000 Sb.
000014487 653__ $$a

000014487 7112_ $$a24th International Congress of Theoretical and Applied Mechanics$$cMontreal (CA)$$d2016-08-21 / 2016-08-26$$gICTAM2016
000014487 720__ $$aPaolucci, Samuel
000014487 8560_ $$ffischerc@itam.cas.cz
000014487 8564_ $$s90562$$uhttps://invenio.itam.cas.cz/record/14487/files/TS.FM04-2.05.pdf$$yOriginal version of the author's contribution as presented on CD,  page 667, code TS.FM04-2.05
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000014487 962__ $$r13812
000014487 980__ $$aPAPER