A review of fundamental research in combustion stabilization for hypersonic airbreathing
propulsion is presented. Combustion in high-speed airbreathing propulsion systems …

Due to the wide flammability range and low ignition delay of Hydrogen, it can burn rapidly
and generate a large amount of thrust. It is for this reason alone that many researchers have …

The major hurdle in augmenting the performance of supersonic engines is the appropriate
distribution of injected fuel within the supersonic chamber. That's why SST k− ω model is …

With the advancement of the air-breathing propulsion system, the supersonic vehicle
technique has drawn a significant interest worldwide. The mixing and combustion process in …

At present, the critical issue related to design of scramjet engine is to achieve efficient mixing
between the air and fuel. Among the several fuel injection strategies, cavity flame holder is …

Achieving efficient fuel-air mixing is a crucial problem for the design of scramjet engines.
Due to the very short residence time of the fuel within the scramjet combustor for typical flight …

The dual-mode scramjet combustor is a promising candidate for the combined cycle engine
of the hypersonic airplane, and the flame propagation and stabilization process in the dual …

Increasing the fuel mixing performance in the combustor of scramjet substantially improves
the overall efficiency of the scramjet engine. In this article, computational fluid dynamic is …

Conventional fuels for vehicular applications generate hazardous pollutants which have an
adverse effect on the environment. Therefore, there is a high demand to shift towards …

Stringent emission norms being followed throughout the world increases the demand for
clean and green fuels. Gaseous fuels like compressed natural gas (CNG), liquefied …