Abstract
In this study, the design, analysis, and production of an unmanned aerial vehicle (UAV) was carried out using SLS (Selective Laser Sintering) production technology. Herein, a multidisciplinary project was realized on the four different aircraft models supported by CFD analysis and the results during the taxing were compared using flow parameters. We observed that according to the numerical study, the design of the model 4 was the most suitable one among the tested models, which was then further utilized for design viability, in-flight CFD analysis, and for the production using SLS process. Finally, the actual flight test was performed in three different weather conditions, and the results are presented here.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
