 |
 |
 |
|
|
|
[Sponsors] | ||||
April 30, 2021, 05:24
|
2D Supersonic Nozzle
|
#1 |
|
New Member
Join Date: Dec 2020
Posts: 23
Rep Power: 5  |
How can I draw the supersonic nozzle of MD 2.2 with the only throat and exit diameter ( 5 & 7.08 mm) and divergence half-angle of alpha 15 deg in Gambit perfectly? Ref paper geometry in the attachment.
|
|
|
|
|
 |
| Tags |
| gambit, nozzle |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| Pressure Driven Supersonic Flow in Coverging-Diverging Nozzle (Wind Tunnel) | shang2 | OpenFOAM Running, Solving & CFD | 1 | March 1, 2019 05:56 |
| kOmegaSST Boundary Conditions for Supersonic Nozzle | shang2 | OpenFOAM Running, Solving & CFD | 2 | September 17, 2018 14:06 |
| Supersonic Nozzle Exhaust Simulation | mikeh | FLUENT | 0 | May 1, 2014 22:28 |
| C-D nozzle supersonic jet boundary | Gland | FLUENT | 4 | May 24, 2012 01:25 |
| some questions for supersonic channel nozzle | goldenland | FLUENT | 2 | November 4, 2007 22:18 |
Linear Mode
