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DTSTART;TZID=Asia/Shanghai:20221005T170000
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SUMMARY:CFD Simulations of Shock Patterns Downstream of a Rocket Nozzle
DESCRIPTION:The live presentation of this event has already taken place. \nPlease view the PDF slides here or watch the video recording below: \n\n\n \nThis webinar focuses on conducting a computational fluid dynamic simulation to understand the flow patterns downstream of a supersonic Rocket engine. The main objective of this webinar is to demonstrate how computational methods can be used to understand flow patterns within problems that are difficult to simulate experimentally. \nSuccessful rocket design involves accurately estimating the thrust generated by it’s nozzle. The thrust parameter however\, is dependent on the ambient pressure and the pressure within the combustion chamber of the rocket. Developing an experimental set up to accurately measure the thrust produced for a supersonic nozzle is a challenging task. With computational tools\, it is relatively easy to simulate the same flow phenomena on a computer. Once a computational setup is created to replicate a given nozzle profile\, the same setup can be used to understand the nozzle’s performance for varying ambient pressure encountered at different altitudes. The thrust profile thus determined can be used in estimating the rocket’s orbit for a given payload. In the webinar\, we will generate a geometry in Ansys Spaceclaim and generate a structured mesh using blocking technology. The mesh will be solved in Ansys Fluent to capture relevant flow phenomena. \nKey takeaways from this webinar: \n\nUsefulness of simulation in solving problems difficult to reproduce experimentally.\nVisualization of complex flow patterns in a supersonic intake duct.\nUsefulness of Ansys CFD workflow to simulate complex fluid dynamic flow fields\n\nPresenter: Mr Vijay Kumar Veera\, EIT Lecturer. \nVijay Kumar Veera is a qualified Aerospace Engineer with over 11 years of experience in using CFD methodologies to simulate industrial and academic problems. He has obtained an M.Phil degree in Engineering from Cambridge University in UK and has M.Tech and B.Tech degrees from Indian Institute of Technology in Bombay and Madras respectively. His expertise is in capturing Fluid flow phenomena using computational methods. He has worked with major organizations in Australia and UK with Red Bull F1\, Mercedes F1\, Boeing\, Airbus\, Thales\, DSTO\, Fisher & Paykel some of the notable clients. \nIn his current role as a Unit lecturer and Course Coordinator at EIT\, he has been instrumental in developing lecture materials for teaching Advanced fluid dynamics and Aerodynamics units for students pursuing Master of Mechanical Engineering. His passion is in teaching computational fluid dynamic techniques for solving real world problems\, which are becoming highly popular with professional engineers wanting to advance their careers to the next level. He is a passionate educator and an advocate for using real world examples in the classroom. \n\nJoin us to learn more at this must-attend event for engineering professionals and aspiring engineers alike. \nReserve your spot at this free webinar today! \n\nThe webinar will be recorded and will be sent out to registered attendees afterwards.\nA certificate of attendance will be provided to attendees who request one near the end of the live webinar session.\n\nPlease note: the time stated on this event is in Australian Western Standard Time (AWST). You will need to convert this to your own time zone.
URL:https://www.eit.edu.au/event/cfd-simulations-of-shock-patterns-downstream-of-a-rocket-nozzle/
LOCATION:Online
CATEGORIES:Technical Engineering Topics Webinar
ATTACH;FMTTYPE=image/jpeg:https://www.eit.edu.au/wp-content/uploads/2022/09/iStock-1165749633.jpg
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