Control of Flow Separation Over Airfoil using Electromagnetic Force
Main Article Content
Abstract
To cater to the needs of air transportation, different wings for varying flight regimes for subsonic and supersonic were developed. However, the use of a particular wing is limited to only for a specific regime. Present work attempts to establish a relation between aerodynamic and electromagnetic energies associated with a wing. The understanding of aerodynamic and electromagnetic as a whole will lead to the idea of developing an autonomous wing. Experimental study was conducted on an unsymmetrical wing (with airfoil NACA 25115) with electric current flowing over its surface. The novelty of the work is that the results will be used for designing a wing that adjusts itself according to the flow conditions, eliminating the need for different wing for different flight regimes and flow conditions.
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).