Abstract

The heat transfer properties of catalytic materials at high temperatures has been studied using a method based on the numerical analysis of the thermal viscous boundary layer near the shock-tube end. Major analysis has been carried out in terms of one-dimensional nonsteady flow models. Finally, a very valuable information regarding the characteristics of the thermal boundary layer near the tube and the parameters of catalytic wall materials has been derived from the observed dependence of heat flux and pressure at the shock-tube end as well as reflected shock wave velocity upon time. 12 refs.

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