MOC matlab code for Divergent part nozel design
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Does anyone know how to transfer the data obtained in matlab to anys ??
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 |
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) ?
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CD nozzle design code
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...:) |
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