A number of important effects have been observed in the droplet size transition region in spray combustion systems. In this region, where the mechanism of flame propagation is transformed from diffusive to premixed dominated combustion, the following effects have been observed: (1) maxima in burning velocity; (2) extension of flammability limits; (3) minima in ignition energy; and (4) minima in NOx formation. A monodisperse aerosol generator has been used to form and deliver a well controlled liquid fuel spray to the combustion test section where measurements of ignition energy have been made. The ignition studies were performed on monodisperse n-heptane sprays at atmospheric pressure over a range of equivalence ratios and droplet diameters...
The thesis describes a programme of research to determine ignition energy requirements in flowing ke...
Technology development for propulsion systems of upper stages and reaction control thrusters is driv...
Technology development for propulsion systems of upper stages and reaction control thrusters is driv...
A number of important effects were observed in the droplet size transition region in spray combustio...
Ignition studies were perferred on monodisperse n-heptane sprays at atmospheric pressure over a rang...
A study of spark ignition energy requirements was conducted with a monodisperse spray system allowin...
The ultimate objective of this study is to obtain fundamental information relevant to combustion pro...
Fuel droplets represent strong inhomogeneities that are generally detrimental and intensify the stoc...
The forced ignition process has a stochastic nature, which can be intensified due to turbulence and ...
A two-fluid pneumatic atomizer operating at relatively high liquid and gas pressures produced water ...
In typical liquid-fueled burners the fuel is injected as a high-velocity liquid jet that breaks up t...
An earlier analysis for the combustion response of a liquid monopropellant strand (hydrazine) was ex...
Detailed measurements were made of the structures of turbulent fuel sprays vaporizing in heated airs...
The steady combustion characteristics of droplets were considered in combustion chamber environments...
This thesis presents an extensive study of turbulent air-blasted sprays aimed at advancing the curre...
The thesis describes a programme of research to determine ignition energy requirements in flowing ke...
Technology development for propulsion systems of upper stages and reaction control thrusters is driv...
Technology development for propulsion systems of upper stages and reaction control thrusters is driv...
A number of important effects were observed in the droplet size transition region in spray combustio...
Ignition studies were perferred on monodisperse n-heptane sprays at atmospheric pressure over a rang...
A study of spark ignition energy requirements was conducted with a monodisperse spray system allowin...
The ultimate objective of this study is to obtain fundamental information relevant to combustion pro...
Fuel droplets represent strong inhomogeneities that are generally detrimental and intensify the stoc...
The forced ignition process has a stochastic nature, which can be intensified due to turbulence and ...
A two-fluid pneumatic atomizer operating at relatively high liquid and gas pressures produced water ...
In typical liquid-fueled burners the fuel is injected as a high-velocity liquid jet that breaks up t...
An earlier analysis for the combustion response of a liquid monopropellant strand (hydrazine) was ex...
Detailed measurements were made of the structures of turbulent fuel sprays vaporizing in heated airs...
The steady combustion characteristics of droplets were considered in combustion chamber environments...
This thesis presents an extensive study of turbulent air-blasted sprays aimed at advancing the curre...
The thesis describes a programme of research to determine ignition energy requirements in flowing ke...
Technology development for propulsion systems of upper stages and reaction control thrusters is driv...
Technology development for propulsion systems of upper stages and reaction control thrusters is driv...