|
[Sponsors] |
If flying a supersonic tube, how to get rid of the flow through the inner duct |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
October 19, 2023, 14:09 |
If flying a supersonic tube, how to get rid of the flow through the inner duct
|
#1 |
New Member
Kevin
Join Date: Jul 2023
Posts: 12
Rep Power: 3 |
Hello,
I am simulating supersonic flow of some vehicle in the shape of a tube, similar to a straw shape. The normal shock inside the tube (inner duct) creates flow spillage, which spills out in the front of the tube (inlet) and causes a huge increase in drag. I want to get rid of the flow through the duct to get rid of that shock, which therefore gets rid of the increase in drag. How should I go about this? New boundary conditions? |
|
Tags |
supersonic |
Thread Tools | Search this Thread |
Display Modes | |
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Is recirculating flow is free vortex or forced vortex? | FluidKo | Main CFD Forum | 11 | July 21, 2022 07:21 |
Issues on the simulation of high-speed compressible flow within turbomachinery | dowlee | OpenFOAM Running, Solving & CFD | 11 | August 6, 2021 07:40 |
[How to obtain supersonic flow inside a supersonic wind tunnel ?] | yx213 | Siemens | 1 | September 17, 2014 14:52 |
back pressure at exit for supersonic flow | BigFrank | FLUENT | 6 | April 24, 2014 16:13 |
analyzing the temperature of fliud (air) flow inside an underground duct. | arshbunny | CFX | 9 | April 3, 2014 09:52 |