Effect of Secondary Nozzle Angle Orientation on Subsonic Coaxial Jet Mixing
Main Article Content
Abstract
In this article, the effects of Secondary Nozzle Angle Orientation (SNAO) on subsonic coaxial jet decay have been studied numerically. The SNAO cases chosen for the study were 15(, 30( and 45( respectively and were compared. The analysis is focused on the jet mixing characteristics of the mentioned nozzles by studying the Mach number decay curves along with the contours of Mach number and density. The findings indicate that the 45° converging angled secondary jet case exhibits, superior reduction in potential core length compared to other configurations in the study. Additionally, the angle variation of the coaxial nozzle significantly impacts jet mixing inhibition characteristics. Coaxial jets with a 45( orientation demonstrate considerably higher mixing compared to those with 15( and 30( orientations.
Article Details
Issue
Section
Articles
This work is licensed under a Creative Commons Attribution 4.0 International License.
Authors who publish with this journal agree to the following terms: a. Authors retain copyright and grant the journal right of first publication, with the work two years after publication simultaneously licensed under a Creative Commons Attribution License that allows others to share the work with an acknowledgement of the work's authorship and initial publication in this journal. b. Authors are able to enter into separate, additional contractual arrangements for the non-exclusive distribution of the journal's published version of the work (e.g., post it to an institutional repository or publish it in a book), with an acknowledgement of its initial publication in this journal. c. Authors are permitted and encouraged to post their work online (e.g., in institutional repositories or on their website) prior to and during the submission process, as it can lead to productive exchanges, as well as earlier and greater citation of published work (See The Effect of Open Access).