-
-
November 13, 2018 at 6:34 am
rumth
SubscriberI am facing some troubles to run compressible flow in a nozzle.
1. I am using mass flow rate boundary condition at inlet and providing static pressure 8.56 atm. But from contour, the static pressure showing    4.86 atm. How FLUENT calculating this pressure? Also static pressure showing negative, how to solve the issue?
2.  If I change the mass flow rate or pressure, the inlet and outlet Mach number after converged remains same for all cases. This is not expected. Why this is happening?
Â
Raju.
-
November 13, 2018 at 1:53 pm
Karthik Remella
AdministratorHello,
Mass flow rate inlet boundary condition allows for specification of mass flow rate. Here, the total pressure is not fixed and will rise to whatever value is necessary based on the computed static pressure. This value of static pressure is dependent on the mass flow rate specified. In the boundary condition panel. The static pressure (you specified) will be used only when your flow is supersonic or if you are initializing the solution from your mass flow inlet boundary condition. This value will be ignored if your flow is subsonic.Â
Static pressure is always specified relative to the operating pressure. Unless you make a change, operating pressure is always set to 1 atm. Negative values of static pressure, if your operating conditions are set to 1 atm, are not an issue. It just means that your absolute pressure is lower than 1 atm.
Please have a look at sections 6.3.5 - Mass-flow inlet boundary conditions, 6.3.4.1.7 - defining static pressure, and 7.14.1 The significance of operating pressure from the Fluent Users Guide. This will provide you with a better understanding.
I hope this helps.
Best Regards,
Karthik
-
November 13, 2018 at 6:07 pm
rumth
SubscriberI am initializing the solution from your mass flow inlet boundary condition. Is there any option to see the specified static pressure at the contour?
Â
Thanks.
-
November 13, 2018 at 6:47 pm
Amine Ben Hadj Ali
Ansys EmployeePlease read the detailed answer of my colleague more thoroughly. The specified pressure is only used for supersonic cases or is parsed into initialization if you say "initialize" from that "inlet". You won't see it in any contour plot (only by chance)
-
- The topic ‘About pressure’ is closed to new replies.
- air flow in and out of computer case
- Varying Bond model parameters to mimic soil particle cohesion/stiction
- Eroded Mass due to Erosion of Soil Particles by Fluids
- Centrifugal Fan Analysis for Determination of Characteristic Curve
- Guidance needed for Conjugate Heat Transfer Analysis for a 3s3p Li-ion Battery
- I am doing a corona simulation. But particles are not spreading.
- Issue to compile a UDF in ANSYS Fluent
- JACOBI Convergence Issue in ANSYS AQWA
- affinity not set
- Resuming SAG Mill Simulation with New Particle Batch in Rocky
-
3862
-
1414
-
1220
-
1118
-
1015
© 2025 Copyright ANSYS, Inc. All rights reserved.