Issue 29
S. Terravecchia et al., Frattura ed Integrità Strutturale, 29 (2014) 61-73; DOI: 10.3221/IGF-ESIS.29.07
u
, u c1
x y n u n
g
0
x
x
(19a,b,c,d)
u c2
g
,
0
y
y
with c1 and 2 c being the wideness of the displacements; - for the case of rigid motion of rotation having width f (Fig.2b) f
(20a)
u
x y n u n
u
f y
g
f n
x
x
y
(21b,c,d,e)
u f x
g
f n
y
y
x
y
y
x u c1 =
f= f
y u c2 =
x
x
a) b) Figure 2 : Rigid motions: a) translation, b) rotation.
Observations about the load vector as a consequence of the rigid motion 1) If the solid is subject to a rigid motion of translation (Fig.2a) having assigned values of the displacements c1 and 2 c , one has U 0 and G 0 but the total load vector has to be u g L L L 0 with
*
) A C a
(
0 0
ut
ut
, u tc
) U
(
(22)
L
u
*
A a
gt
, g tc
A
0 0
ur
( ) G
(23)
L
A C
g
gr
gr
and as a consequence the solution vector X has to be null. 2) If the solid is subject to a rigid motion of rotation (Fig.2a) having assigned rotation vector
f φ , in the generic node
i one has
i i G φ n φ s 0 i
i i U r φ 0
(24a,b)
with s being respectively the unit normal and tangent vectors to the boundary elements on which the node i lies, but the total load vector has to be i r vector distance between the instantaneous center of rotation and the node i , i n e i
u g L L L 0 with
67
Made with FlippingBook - Online Brochure Maker