Subsonic Jet Spread Characteristics Normal to Tab Axis for Semi Circular Corrugated Tabs
Main Article Content
Abstract
This work involves an experimental study of the spread characteristics normal to tab axis for a Mach 0.8 subsonic jet using triangular tabs with semi-circular corrugations. The semi-circular corrugation is made on the equally leaning sides of trilateral tabs that are precisely kept 180deg apart at the convergent nozzle’s exit. The jet spread examination was conducted at several axial points as 0.3, 0.5, 0.7, 1 and 3 fractions of the jet distance. An open jet facility is used to perform the investigations and to carry out the pressure measurements. From the results, it is found that even a small variation in the location of the corrugations on the leaning side of triangular tab can affect the jet spread and improves the jet mixing process.
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).