Supersonic Nozzle Study in Ansys Fluent

This course teaches how to simulate supersonic nozzles and combustion in rocket engines using Ansys Fluent. The learning outcomes include understanding supersonic flow behavior and simulating combustion processes. The course covers skills such as setting up simulations in Ansys Fluent and analyzing results. The teaching method involves practical demonstrations and step-by-step guidance. The intended audience for this course includes engineering students, researchers, and professionals interested in computational fluid dynamics and aerospace engineering.