[SURENDRA SONI]

Originally Posted by zino

anyone found the code?n does it really work? I also need it. please email at "05021992sssoni@gmail.com"

Thanks in advance.

[Sorwar22]

I have used the method of characteristics method to create the divergent section of the nozzle i no want to run the simulation in ansys fluent after slight modification in design modeller. Does anyone know how really stuck on this for quite some time any help would be appreciated thank you in advance
reagrds
sorwar

[mkhm]

Did anyone found any code working properly to design the 2D supersonic nozzle ? If yes, do you get at the outlet the Mach number that would corresponds to 1D isentropic flow's Mach number (function of the the area ratio A_outlet/A_throat and Gamma parameter that you use to get 2D geometry) ?

[Sorwar22]

Originally Posted by mkhm

Did anyone found any code working properly to design the 2D supersonic nozzle ? If yes, do you get at the outlet the Mach number that would corresponds to 1D isentropic flow's Mach number (function of the the area ratio A_outlet/A_throat and Gamma parameter that you use to get 2D geometry) ?

Look up gas dynamic equations it will allow you to build the profile using the equations related. I did this on Excel which allowed me to find the Mach numebr throughout the nozzle both inlet and outlet.

[AMANJ]

Hi
I am a beginner in nozzle design,

I want to design a supersonic nozzle with characteristics approach
if you have any code for nozzle design, send me please : aminanjam@gmail.com



thank you...