Can you plz let me know how to calculate boundary conditions (inlet and outlet) for given chamber pressure (P0) and nozzle expansion ratio (AR)? Need to get Normal Shock in it. Appreciate your help.
Generally, there is no three-dimensional effect on axis-symmetric structures, so they can be easily simulated in 2D. This video helps students in Gas Dynamics to study Ansys Fluent. Due to the license limitations and simulation time, we work in 2D. Three-dimensional simulations are made just on the final project.
Thank you very much, it's just what I needed for my project!
Hello can you provide the code of MOC or shape how you get the coordinates. we are watching and unable to practice the model
Hello. The coordinates are present in the comments in the first part of this playlist.
Can you plz let me know how to calculate boundary conditions (inlet and outlet) for given chamber pressure (P0) and nozzle expansion ratio (AR)? Need to get Normal Shock in it.
Appreciate your help.
Hello. Such a calculation may be found in the textbook of Anderson "Fundamentals of Aerodynamics", chapter 10
Hello sir can u please make a video on same 3d nozzle
Generally, there is no three-dimensional effect on axis-symmetric structures, so they can be easily simulated in 2D. This video helps students in Gas Dynamics to study Ansys Fluent. Due to the license limitations and simulation time, we work in 2D. Three-dimensional simulations are made just on the final project.