2023
DOI: 10.14429/dsj.73.17893
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Studies of Jet A1 Fuel Atomization Through Non Circular Orifices

V. Vani Pooja,
Rajiv Kumar

Abstract: The performance of the liquid rocket engine depends on the atomization behavior of the fluid being injected into the combustion chamber. Generally, a plain injector with a circular orifice has been used in the injector, but it has the disadvantage of having a low spray cone angle. The breakup length, mean droplet diameter, and Sauter mean diameter is also higher. Thus, to overcome these drawbacks, non-circular orifices have been utilized in the present study. The shapes used for non-circul… Show more

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