Card 9 - QNODE Heat Load Definition
This optional card defines heat loads for elements.
Parameters: KODE
, N1
, T1
,
T2
, T3
, T4
,
T5
KODE
KODE
is the code QNODE
(or 1)
N1
N1
is an element number, or a group name.
T1
T1
is the specified heat load, or heat load/area, or heat
load/volume into N1
.
T2
T2
may be:
- the specified time when the heat load occurs (this option is not recommended).
T2
may not be < 0, unlessT2
= -99990. - the code
CONSTANT
(or -99990) for constant heat loads. IfT2
is blank it defaults toCONSTANT
. - the form
Tn
(e.g.T6
), where n is a table number specified by TABTYPE and FIELDTYPE Cards, and table n specifies a heat load multiplier. The total heat load will then be equal to the value interpolated from tableTn
, timesT1
, times the geometrical multiplying factor computed fromT3
. - the form
En
(e.g.E6
), where n is an expression number specified by EXPRESSION card, and expression n specifies a heat load multiplier. The total heat load will then be equal to the value evaluated from expressionEn
, timesT1
, times the geometrical multiplying factor computed fromT3
.
T3
T3
may be:
- blank,
ABSOLUTE
, or 0.T1
is the heat load into elementN1
. AREA
(or 1E36).T1
is the heat load per unit area into elementN1
.LENGTH
(or 4E36).T1
is the heat load per unit length into elementN1
. This is applicable to beam elements only.TOTAL
(or 2E36). The heat load is redistributed among the elements of groupN1
in proportion to their areas or volumes.VOLUME
(or 3E36).T1
is the heat load per unit volume into elementN1
. For planar and beam elements the volume is calculated by multiplying the length or area by the cross-sectional area or thickness.
For T3 = TOTAL
heat load is computed as:
where:
- AV(I) is either the volume (for solid elements) or area of element I (for
shells and beams), or unity (for non-dimensional element), where I is a member
of the
N1
group. All the elements of groupN1
must be of the same type, i.e. solid and non-solid elements may not be mixed. - Q(I) is the heat load to element I, which is a member of the group
N1
. - Ω(T2,I) is the interpolated variable where
T2
is a table.
If T2
is a spatial table (field or EID dependent), then
Q(I) is calculated with a weighting factor Ω(I) interpolated from
this table:
When
T2
includes a reference to an expression, either directly or
through a table, then each spatial field, referenced in that expression is
normalized by a factor that makes the area-weighted average of that field equal to
one. The averaging is performed over the N1
element group.
If
N1
is a single element, the heat load is applied to the
element.
T4
T4
specifies the layer for multilayer elements. Non-homogeneous
multilayer elements are specified on LAYER Cards, homogeneous multilayer elements
are specified on PROP Cards.
0
, blank, orTOP
, the element is not multilayer or heat load is applied to the top layer.MIDDLE
– heat load is applied to the middle layer.BOTTOM
– heat load is applied to the bottom layer.ALL
– heat load is applied to all the layers.SPECIFY
– heat load is applied to theT5
th layer, as counted from the bottom layer.T4
= 1 is the same asT4
=BOTTOM
.
T5
T5
is the layer number for T4
=
SPECIFY
.
Code example
QNODE 14 30 CONSTANT
$ HEAT LOAD OF 30 IS ADDED TO ELEMENT 14
QNODE 14 30 8 AREA
$ A HEAT LOAD = 30*AREA(14) IS ADDED TO ELEMENT 14 AT TI
Notes
Orbital radiative heat loads calculated from geometry are automatically summed by the MEREL module with those specified on QNODE Cards.
A T2
parameter value other than CONSTANT
or a table
number is not recommended if orbital heat loads are also calculated. This is because
it is necessary to match with T2
all the orbital time parameters on
QNODE Cards, otherwise errors can result.
To work around this problem, it is recommended that you specify time-dependent heat loads on tables with INTERP, TABTYPE, and FIELDTYPE Cards, or with user-written subroutines. This will avoid the problem of matching all the time values if orbital heat loads are also calculated.