To achieve stable combustion within supersonic combustors, the strut-based mixing
augmentation techniques are commonly employed. Large Eddy Simulations (LES) are …

Insight into supersonic combustion characteristics of thermally cracked fuels in a scramjet
combustor is crucial for the development of next-generation supersonic flight vehicles. In the …

A scramjet engine offers a potential route to achieve supersonic speeds using airbreathing
engines. Achieving proper mixing and combustion poses a challenge due to the supersonic …

The present study numerically investigates the combustion characteristics and performance
of a direct-connect gaseous hydrogen-fueled scramjet combustor depending on the injector …

As the Mach number increases, the local static temperature gradually approaches the
characteristic gas vibration/dissociation temperature, and significant thermo-chemical …

The request for faster and greener civil aviation is urging the worldwide scientific community
and aerospace industry to develop a new generation of supersonic aircraft, which are …

Scramjet propulsion holds promise for high-speed travel and reusable satellite launches, but
fuel combustion at supersonic speeds presents a challenge. Limited retention time hinders …

In this study, a solid fuel combined cycle engine concept based on the distributed
combustion and the self-adaptive thermal choking is proposed, which can operate effectively …

With the overwhelming trend of fast and economic aviation, it is becoming increasingly
difficult for fuel to burn stably and efficiently in a constrained space and time period in the …

Here we report on reactive Large Eddy Simulations (LES) of flow and combustion in the US
Air Force Research Laboratory Research Cell 19 cavity-based scramjet combustor. This …