PSI - Issue 58
Victor Rizov et al. / Procedia Structural Integrity 58 (2024) 150–156 V. Rizov / Structural Integrity Procedia 00 (2019) 000–000
153
4
a A ( ) ( ) A
N
dA
,
(12)
M
z dA 1
,
(13)
a
where N is the axial force, M is the bending moment, A is the cross-section area. The MatLab is used to solve (12) and (13). In frame members, 2 3 B B and 3 4 B B , the curvature and the coordinate of neutral axis are determined in a similar way. We obtain the damping energy by integrating the damping energy density, u . The latter is determined by formula (14).
1
1
1 41
n
n H n
C
u
C a
.
(14)
1
C C C n
We give an account of the influence of the temperature, T , on the damping by changing
C H . For this purpose,
we apply the following relations (Narisawa (1987)):
t T
T
H t C
H
0 0
,
(15)
CT
T
1
0
C T T C T T q P
lg
,
(16)
q
T
R
C H at a reference temperature, q T is a constant. The rest of the constants involved in
0 CT H
where
is the value of
8.86 P C ,
101.6 R C and
/( ) 1 1 0 0 T T
(15) and (16) are
(Narisawa (1987)).
We apply formula (17) for deriving the damping energy, U , in the frame.
2 3 B B B B U U U U 1 2
,
(17)
3 4
B B
where the subscripts, 1 2 BB , 2 3 B B and 3 4 B B , refer to the corresponding frame member (Fig. 1). Formula (18) is used to determine the damping energy in frame member, 1 2 BB .
U B B V B B ) ( 1 2 1 2
udV
,
(18)
where V is the volume of this frame member. The damping energies in frame members,
2 3 B B and 3 4 B B , are found-out by formulas (19) and (20), i.e.
U 2 3 V B B B B ) ( 2 3
u dV B B 2 3
,
(19)
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