A production gas turbine combustor swirl cup and a 3x-scale model, both featuring co-axial, counter-swirling air streams are characterized at atmospheric pressure and in the absence of reaction. Spatially-resolved measurements of continuous phase (gas in the presence of spray) and droplet size and velocity are acquired downstream of the production and 3x-scale swirl cups by using two-component phase Doppler interferometry. The effect of scale on the behavior of the continuous phase and droplets is investigated by comparing the continuous phase velocity and droplet size and velocity at geometrically analogous positions. The continuous phase flow field scales well at the exit of the swirl cup. Farther downstream, differences occur which are d...
In the present study flow conditions in the near nozzle region of the combustion chamber have been i...
In liquid-fueled combustion, the interaction of spray droplets with surrounding turbulent air flow i...
A pressure—swirl fuel nozzle generating a hollow—cone spray with nominal cone angle of 30 degrees is...
A production gas turbine combustor swirl cup and a3× -scale model (both featuring co-axial, counters...
The two-phase flow downstream of a production gas-turbine engine combustor fuel injection system (i....
A liquid fuel air-assist atomizer is characterized in both an isothermal spray chamber and a swirl-s...
For swirl-stabilized gas turbine combustor, liquid fuel distribution in the near field dictates loca...
The turbulent particle dispersion is investigated with regard to the two-phase flow of fuel spray an...
A model laboratory reactor is presented and characterized for the study of spray-fired combustion in...
The kerosene spray generated by a pressure swirl fuel nozzle embedded in a swirling airflow in a swi...
The application of two-component interferometry is described for the spatially-resolved measurement ...
The dispersion of droplets and mixing of evaporated gases in a swirl stabilized gas turbine combusto...
Abstract: Coupling of spray with the coherent structures of highly turbulent flow has been a long-st...
Drop size and velocity measurements in a confined, swirl-stabilized, reacting spray are presented. T...
The effects of swirl and vaporization on droplet dispersion are investigated in the near region of a...
In the present study flow conditions in the near nozzle region of the combustion chamber have been i...
In liquid-fueled combustion, the interaction of spray droplets with surrounding turbulent air flow i...
A pressure—swirl fuel nozzle generating a hollow—cone spray with nominal cone angle of 30 degrees is...
A production gas turbine combustor swirl cup and a3× -scale model (both featuring co-axial, counters...
The two-phase flow downstream of a production gas-turbine engine combustor fuel injection system (i....
A liquid fuel air-assist atomizer is characterized in both an isothermal spray chamber and a swirl-s...
For swirl-stabilized gas turbine combustor, liquid fuel distribution in the near field dictates loca...
The turbulent particle dispersion is investigated with regard to the two-phase flow of fuel spray an...
A model laboratory reactor is presented and characterized for the study of spray-fired combustion in...
The kerosene spray generated by a pressure swirl fuel nozzle embedded in a swirling airflow in a swi...
The application of two-component interferometry is described for the spatially-resolved measurement ...
The dispersion of droplets and mixing of evaporated gases in a swirl stabilized gas turbine combusto...
Abstract: Coupling of spray with the coherent structures of highly turbulent flow has been a long-st...
Drop size and velocity measurements in a confined, swirl-stabilized, reacting spray are presented. T...
The effects of swirl and vaporization on droplet dispersion are investigated in the near region of a...
In the present study flow conditions in the near nozzle region of the combustion chamber have been i...
In liquid-fueled combustion, the interaction of spray droplets with surrounding turbulent air flow i...
A pressure—swirl fuel nozzle generating a hollow—cone spray with nominal cone angle of 30 degrees is...