Ansys Fluent analysis of C D nozzle

[@gurughantalhostelteam9148]

This is very very helpful to us 🙏🙏

[@AZAHARMONDAL-t5l]

why static pressure is displaying as negetive?

[@runitvg]

wonderful lesson

[@المختارعبدالرزاقفرحان]

Could you make another video for the same geometry but at conditions that give a normal shock at the divergent section?

[@gurughantalhostelteam9148]

Thanks sir

[@shravanmishra4429]

Many many thanks. What is NPR(nozzle pressure ratio)? and What is NPR in this simulation?

[@antoine1407]

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

[@Cre8ive_spark]

Sir will you please send the paper link from which paper u have taken these dimensions

[@Rafael-es3go]

Why use air? you should specify a propellant, no?

[@yashwanth2730]

Sir could you please upload report of this project

[@i-jg3kc]

"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?