Abstract A technique for calculating the two-phase flows in the pneumatic injector of the aircraft engine is developed based on solving the model problem, namely, on verification of the two-phase flow model by means of solving the problem of liquid column disintegration under the effect of an incident airflow. We determine the turbulence models that satisfactorily describe the biphase flow processes.
A technique for numerical modeling of liquid film disintegration in the pneumatic injector of aircraft engines
Russian Aeronautics ; 60 , 1 ; 97-102
2017-01-01
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Triaxial Swirl Injector Element for Liquid-Fueled Engines
Online Contents | 2010
Engineering Index Backfile | 1932
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