The primary objective of a liquid fuel injection system is to provide the combustion chamber with the proper amount of fuel and with a spatial pattern that will result in efficient combustion over the entire flight path of the ramjet. In [1], empirical methods for designing fuel injectors were defined. In this work, the approach of Wu [2] to calculate the breakup time of the jet, the correlation of Lefevbre [3] for the average diameter of the droplets of fuel, the study of Turns [4] to calculate the time of vaporization of the droplet and the data processed by Kundu, Colket and Fuller [5–7] for the delay have been selected to provide guidelines to injector design.
Injector Design Guidelines
SpringerBriefs in Applied Sciences
2021-01-30
11 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Electronically Controlled Injector Design Technologies
Wiley | 2019
|An optimum fuel injector design
Kraftfahrwesen | 1999
|Fundamental problems of injector design.
NTRS | 1968
|Fluorescence imaging advances fuel-injector design
British Library Online Contents | 2003