my flow has a mach numer greater than 1 at the inlet. I need to impose pressure inlet boundary condition, how could I do? Should I set the pressure in Gauge Pressure or using supersonic inlet option? Thanks for your tutorial
"Error: > (greater-than): invalid argument [2]: wrong type [not a number] Error Object: 1.#qnan Error: WorkBench Error: Could not handle event: SolutionStatusUpdate Error Object: #f" sir I am getting error like this..... can u tell me how to solve this?
This is very very helpful to us 🙏🙏
wonderful lesson
Many many thanks. What is NPR(nozzle pressure ratio)? and What is NPR in this simulation?
Thanks sir
Could you make another video for the same geometry but at conditions that give a normal shock at the divergent section?
my flow has a mach numer greater than 1 at the inlet. I need to impose pressure inlet boundary condition, how could I do? Should I set the pressure in Gauge Pressure or using supersonic inlet option? Thanks for your tutorial
Sir will you please send the paper link from which paper u have taken these dimensions
Why use air? you should specify a propellant, no?
"Error: > (greater-than): invalid argument [2]: wrong type [not a number]
Error Object: 1.#qnan
Error: WorkBench Error: Could not handle event: SolutionStatusUpdate
Error Object: #f" sir I am getting error like this..... can u tell me how to solve this?
Sir could you please upload report of this project