3D Super sonic Nozzle Internal flow simulations || Shock diamonds || RANS equation || ANSYS Fluent

[@jameslee4221]

Where are you getting the hydrogen combustion thermal properties from at 4:23?

[@akshay9762]

Why didnt you select transient ? Also Density based solver right ?

[@md.shahinurrahman747]

One silly Question, what is representing the cylindrical shape that is started from the exit face of the nozzle?

[@zaheddastan4771]

I think he's trying to simulate the environment with that cylinder. Otherwise, the software would only show you the fluid inside the nozzle, not after it.

[@user-oc6ne8xg5b]

Please share the related geometry file. I really need it. Thank you

[@SMBhai29]

Can you share the geometry file?

[@al-falaah479]

WHY SUDDEN EXPANSION AFTER NOZZLE EXIT

[@kaisa_nd]

это особенность сверзвукового потока, если скорость меньше скорости звука при сужении потока скорость растет, давление будет падать. Когда скорость превышает 1 М (supersonic) происходит наоборот, при расширении потока скорость увеличиться и также уменьшится давление. Данное сопло Лаваля это и делает. на входе имеем скорость М 1

[@alializadeh8195]

مرسی

[@xToFaN21x]

Where is geometry file bro

[@xToFaN21x]

Are u kidding me?

[@luiswalsh4260]

what is the name of this software?

[@Andres-gr3us]

Ansys Fluent

[@lucamucciante6977]

can u share the geometry file? plis

[@cfdmantra3078]

It's general Nozzle and created as surface in CAD software

[@kaalarudra8329]

Super