Injector

Quantum mechanics

Mixing (physics)

Turbulence

Engineering

Aerospace engineering

Materials science

Mach number

Airflow

Coaxial

Nozzle

Jet (fluid)

Jet fuel

Mechanical engineering

Thermodynamics

Supersonic speed

Physics

Organic chemistry

Combustion

Combustor

Chemistry

Mechanics

Scramjet

Fuel injection

International Journal of Hydrogen Energy

In this research study, a computational method is applied to examine the impacts of coaxial hybrid air and fuel jets on fuel mixing at the supersonic cross-flow of Mach = 4. This study examined the coaxial air and fuel jet effects on main parameters i. e. circulation, mixing efficiency, and fuel penetration. Computational Fluid Dynamic is employed for the modelling of the coaxial jet at cross supersonic flow. Reynolds Average Navier-Stocks equations with SST turbulence model for achieving hydrodynamic feature of the main model. Impacts of air-jet pressure and nozzle configurations on fuel distribution are also presented and the main effective factors for efficient fuel mixing condition are explained. Our results disclosed that injection of coaxial air and fuel jets at supersonic cross airflow significantly improves the fuel penetration and mixing inside the combustion chamber. Flow study analysis shows that the coaxial injector augments the spiral feature of the fuel jet, which surges fuel mixing downstream. Our circulation analysis confirms that circulation strength increases in far away from an injector by the injection of a coaxial air jet.

Effect of hybrid coaxial air and hydrogen jets on fuel mixing at supersonic crossflow