Because of increased heat production or reduction in effective surface area for heat
exclusion, modern electronic equipment typically confronts thermal critical difficulties. This …

The nonlinear convective flow of kerosene-Alumina nanoliquid subjected to an exponential
space dependent heat source and temperature dependent viscosity is investigated here …

A one-dimensional model of the cooling process occurring in a hybrid-rocket nozzle working
with cryogenic oxygen flowing through helical channels is addressed in this work. Although …

The combustion chamber wall surface of a hydrogen fuel rocket engine is exposed to an
exceptionally high heat flux. To effectively mitigate the temperature of these overheated …

For rocket cycles involving electric pumps, gas generators, expanders, and staged
combustion, a thermal recycling method is proposed to provide a more realistic simulation of …

The hydrogen fuel rocket engine combustion chamber wall is very small and suffers high
combustion temperature and heat rates. To effectively reduce the temperature of these …

Coolant flow modeling in regeneratively cooled rocket engines fed with turbo machinery is a
challenging task because of the high wall temperature gradient, the high Reynolds number …

IN ORDER to optimize combustion process and ensure integrity of thrust chamber there is a
need to perform a comprehensive thermal analysis, it is especially important for the design …

Microchannel cooling provides an efficient thermal management method for regenerative
cooling systems of advanced areo engines. In this study, a prototype combustor with …

The structure of the regenerative cooling channels is crucial for high-performance scramjet
engines. To investigate the effect of catalyst coating thickness and aspect ratio on the …