Film cooling in combination with regenerative cooling is presently considered as an efficient
method to guarantee safe operation of liquid rocket engines having higher heat flux …

Serpentine nozzles more easily deform and damage due to high-temperature airflow
because of their multi-bend channel configuration. Therefore, film cooling technologies …

Ratio of static pressure (RSP) is a critical factor affecting the development of supersonic
cooling film flow field. To give a good account of flow characteristics and physical …

FILM-COOLING is an active cooling strategy involving the continuous injection of a thin layer
of fluid near a wall to provide thermal protection from a hot-gas flow. It is widely used in gas …

The flow field associated with cylindrical coolant jets inclined in tangential and azimuthal
direction employed inside a circular pipe has been studied. Numerical results are compared …

The current work presents an experimental parametric study on tangential, supersonic film
cooling in the expansion part of a conical nozzle. For simulating rocket-engine-like hot gas …

In this study, a numerical study was performed to elucidate the influence of triangular with
concave edge shaped (TCES) ramp on film cooling effectiveness (FCE) and flow …

FILM cooling is an important technique used for protecting surfaces that are exposed to the
hot combustion gases. It is accomplished by injecting a layer of coolant fluid between the …

This study is devoted to the characterization and analysis of the flow field and heat transfer
in oxygen/methane liquid rocket engines. Attention is focused on the hot gas side of the …

Oxygen/methane propellant combination has recently gained interest for space propulsion
as proved by the inclusion of its study in the European Community 7th Framework Program …