|
[Sponsors] |
![]() |
![]() |
#1 |
New Member
Imran Rasheed
Join Date: Oct 2018
Posts: 3
Rep Power: 7 ![]() |
hello all,
I am simulating a transverse jet in supersonic cross flow. I am giving mass flow inlet bc at the jet inlet. I am trying to achieve M=1 at jet exit and 1.5 at cross flow inlet. But after the simulation my jet M is going to 1.6. I cross checked the boundary condition after the simulation and everything seems good except the density at jet inlet. i dont understand what is the problem. I used blocking method for meshing. |
|
![]() |
![]() |
![]() |
Tags |
boundary condition, fluent, jet injection, mach number, supersonic flatplate |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
[snappyHexMesh] snappyHexMesh sticking point | natty_king | OpenFOAM Meshing & Mesh Conversion | 11 | February 20, 2024 09:12 |
Inconsistencies in reading .dat file during run time in new injection model | Scram_1 | OpenFOAM | 0 | March 23, 2018 22:29 |
[foam-extend.org] Foam-extend-3.1 on RHEL: mesh problem | lxwd | OpenFOAM Installation | 4 | March 25, 2017 16:10 |
foam-extend_3.1 decompose and pyfoam warning | shipman | OpenFOAM | 3 | July 24, 2014 08:14 |
[blockMesh] --> foam fatal error: | lillo763 | OpenFOAM Meshing & Mesh Conversion | 0 | March 5, 2014 10:27 |