A heat shield called the thermal protection system (TPS) is an important structure in
hypersonic vehicles as it prevents hot air from entering vehicles and potential impacts from …

To study the thermal behavior in the cracking reaction zone of regeneratively cooled
scramjet cooling channels at different aspect ratios, 3-D model of fuel flow in terms of the …

To study the thermal behavior inside scramjet cooling channels at different aspect ratios, a
three-dimensional model of fuel flow in terms of the fuel real properties is built and validated …

This study, which has been motivated by the recent applications of the cold plate device in
aviation thermal management, reports on physics-based mathematical models derived from …

The working process of an advanced aeroengine such as scramjet with endothermic
hydrocarbon fuel cooling is a chemical recuperative cycle. The design of cooling channel in …

Hypersonic air-breathing propulsion (> Mach 5) based on SCRamjet promotes the
revolutions of both military and civilian applications. However, the engine thermal protection …

Recently, advanced aero-engines have become more and more important in the
development of society, which are expected to be capable of higher and higher flight Mach …

Developing fuel with higher heat sink is widely carried out to meet the cooling requirement
for an airbreathing hypersonic vehicle. However, a Re-Cooled Cycle has been newly …

In scramjet engines, the optimal design of a regenerative cooling channel is critical for
cooling, reducing pressure loss on the walls of the combustion chamber and improving heat …

Advanced aero-engines with higher flying Mach number, like SCRamjets, offer good
solution to the hypersonic propulsion. However, the thermal boundary condition of the …