[EN] Primary breakup of liquid fuel in the vicinity of fuel spray nozzles as utilized in aero-engine combustors is numerically
investigated. As grid based methods exhibit a variety of disadvantages when it comes to the ...
García Galindo, Agustín(Universitat Politècnica de València, 2017-09-28)
[EN] In gas turbine combustors, there is a continuous high velocity airflow in which the fuel is injected by means of an atomizer. Given the high turbulence of the airstream, induced through a swirler, the fuel (also ...