(1)

(2)

(3)

(4)

(5)

(6)

(7)

(8)

(9)

(10)

/MAT/LAW6/mat_ID/unit_ID or /MAT/HYDRO/mat_ID/unit_ID

mat_title

C0

C1

C2

C3

Pmin

Psh

C4

C5

E0

#RADIOSS STARTER

/UNIT/1

unit for mat

                 kg                   m                   s

#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|

/MAT/HYDRO/4/1

AIR

#              RHO_I               RHO_0

                1.22                   0

#                Knu

              1.5E-5

#                 C0                  C1                  C2                  C3

                   0                   0                   0                   0

#               Pmin                 Psh

                   0              101320

#                 C4                  C5                  E0

                 0.4                 0.4              253300

/EULER/MAT/4

#     Modif. factor.

                   0

#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|

#enddata

/END

#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|

1.

Where, for no turbulence, Sij is the deviatoric stress tensor and is the deviatoric strain tensor.

with and E being the internal energy unit reference volume.

 and

with being the perfect gas constant.

  and

with c being the sound speed.

and

and

then:

If P = cst = 0, then l=; so

Where, is the dilatation coefficient, means dilatation, and in this case the parameters C2 and C3 will not be taken into account.

6.	All thermal data () can be defined with keyword /HEAT.

•	for Law 37

•

for Law 6

with

then,

•	PV = cst  for Law 37

•

for Law 6

with

and

then,

Where, E is the energy per unit volume and e is the energy per unit mass.