Material#
The Material section defines the physical properties of the simulated fluid inside the Fluid model. For a gas, this is air by default, and you can edit its viscosity model, thermodynamic (thermally perfect gas) species, and Prandtl numbers. For a liquid, it is water, defined by its density and dynamic viscosity.
Note
The material type (Air or Water) follows the Gas/Liquid selection made in the Operating Condition: choosing Gas exposes the Air parameters, choosing Liquid exposes the Water parameters. The freestream state (velocity, density, temperature, etc.) is still defined in the Operating Condition; the Material section only describes the substance itself.
Available Options#
Air (gas)#
Option |
Description |
Applicable |
|---|---|---|
Dynamic viscosity |
Method used to evaluate the dynamic viscosity: |
always |
Reference viscosity |
Reference dynamic viscosity \(\mu_{ref}\) in Sutherland’s law |
Dynamic viscosity is |
Reference temperature |
Reference temperature \(T_{ref}\) associated with the reference viscosity |
Dynamic viscosity is |
Effective temperature |
Sutherland constant \(S\) |
Dynamic viscosity is |
Value |
A single constant dynamic viscosity |
Dynamic viscosity is |
Thermally perfect gas |
List of species (with NASA 9-coefficient polynomials and mass fractions) defining the temperature-dependent thermodynamics of the gas |
always |
Prandtl number |
Laminar Prandtl number |
always |
Turbulent Prandtl number |
Turbulent Prandtl number |
always |
Water (liquid)#
Option |
Description |
Applicable |
|---|---|---|
Density |
Density of the liquid |
always |
Dynamic viscosity |
Dynamic viscosity of the liquid |
always |
Detailed Descriptions#
Dynamic viscosity (Air)#
Selects how the dynamic viscosity of the gas is evaluated.
Default:
SutherlandOptions:
Sutherland: temperature-dependent viscosity following Sutherland’s law: \(\mu(T) = \mu_{ref} \left(\dfrac{T}{T_{ref}}\right)^{1.5} \dfrac{T_{ref} + S}{T + S}\)Constant: a single, temperature-independent viscosity value.
Reference viscosity#
The reference dynamic viscosity \(\mu_{ref}\) at the reference temperature.
Required when Dynamic viscosity is
SutherlandDefault:
1.716e-5 Pa·s
Reference temperature#
The reference temperature \(T_{ref}\) associated with the reference viscosity.
Required when Dynamic viscosity is
SutherlandDefault:
273.15 K
Effective temperature#
The Sutherland constant \(S\) used in Sutherland’s formula.
Required when Dynamic viscosity is
SutherlandDefault:
110.4 K
Value#
A single constant dynamic viscosity, used instead of the Sutherland model.
Required when Dynamic viscosity is
ConstantExample:
1.825e-5 Pa·s
Thermally perfect gas#
Defines the temperature-dependent thermodynamic properties of the gas through one or more species, each described by NASA 9-coefficient polynomials. By default the gas is a single species named Air whose coefficients reproduce a constant specific-heat ratio \(\gamma = 1.4\) (calorically perfect gas).
Each species is edited from its row (the cog opens the species editor) and exposes the following, all required:
Name: the species identifier (e.g.
N2,O2,Ar).Mass fraction: the mass fraction of this species in the mixture.
Temperature: the lower and upper bounds of a temperature range over which a coefficient set applies. A species can hold several ranges (use Add range).
Coefficients: the nine NASA 9-coefficient polynomial coefficients \(c_1 \ldots c_9\) for the range. They define the non-dimensional specific heat, enthalpy, and entropy:
\(\dfrac{c_p}{R} = c_1 T^{-2} + c_2 T^{-1} + c_3 + c_4 T + c_5 T^2 + c_6 T^3 + c_7 T^4\)
\(c_1\)–\(c_7\) are the \(c_p\) polynomial coefficients, \(c_8\) is the enthalpy integration constant, and \(c_9\) is the entropy integration constant.
Use Add species to add another component: the N2, O2, and Ar presets come pre-filled with standard data, while Custom starts from an empty species.
Notes:
The mass fractions of all species must sum to
1.0. Values within a small tolerance (1e-3) are renormalised automatically; otherwise the input is rejected. This validation matches the Python client.Species names must be unique, and all species must use the same temperature-range boundaries.
Prandtl number#
The laminar Prandtl number of the gas.
Required
Default:
0.72
Turbulent Prandtl number#
The turbulent Prandtl number of the gas.
Required
Default:
0.9
Density (Water)#
The density of the liquid.
Required
Default:
1000 kg/m³
Dynamic viscosity (Water)#
The dynamic viscosity of the liquid.
Required
Default:
0.001002 Pa·s
Note
A liquid is described only by its density and dynamic viscosity; it carries no thermal properties such as thermal conductivity or specific heat. Conjugate heat transfer (CHT) is therefore only available with a gas.
❓ Frequently Asked Questions
Why can’t I run a simulation after I added a species?
The mass fractions of all species must sum to
1.0. After adding a species, adjust the mass fractions so they total1.0(values within a small tolerance are renormalised automatically; larger deviations are rejected and the simulation cannot start).
🐍 Python Example Usage
The material is configured via the material field on the Fluid model.
import flow360 as fl
from flow360 import u
# Default air: Sutherland viscosity, single-species calorically perfect gas (gamma = 1.4)
fluid = fl.Fluid(
material=fl.Air(),
)
# Air with a custom Sutherland model and Prandtl numbers
fluid_custom = fl.Fluid(
material=fl.Air(
dynamic_viscosity=fl.Sutherland(
reference_viscosity=1.716e-5 * u.Pa * u.s,
reference_temperature=273.15 * u.K,
effective_temperature=110.4 * u.K,
),
prandtl_number=0.72,
turbulent_prandtl_number=0.9,
),
)
# Air as a constant-viscosity gas
fluid_constant = fl.Fluid(
material=fl.Air(dynamic_viscosity=1.825e-5 * u.Pa * u.s),
)
# Liquid (water) defined by density and dynamic viscosity
fluid_liquid = fl.Fluid(
material=fl.Water(
name="Water",
density=1000 * u.kg / u.m**3,
dynamic_viscosity=0.001002 * u.Pa * u.s,
),
)