Issue 49
A. Baryakh et alii, Frattura ed Integrità Strutturale, 49 (2019) 257-266; DOI: 10.3221/IGF-ESIS.49.25
where . A general solution of this linear differential equation with constant coefficients takes the following form: 1 2 3 4 ( ) ( ) ( ) ( ) f y C ch y C sh y C ych y C ysh y (13) m l
Then a stress function is determined according to the following expression: 1 2 3 4 sin ( ) ( ) ( ) ( ) x C ch y C sh y C ych y C ysh y
(14)
and the relevant stress components are calculated according to the following formulas:
2
2
2
( ) x C ch y C sh y C sh y ( ) 2 ( )
( ) ych y C ch y 2 ( )
( )
ysh y
sin
x
1
2
3
4
2
y
2
2
( ) x C ch y C sh y C ych y C ysh y ( ) ( ) ( )
sin
(15)
y
1
2
3
4
2
x
2
( ) x C sh y C ch y C ch y ( ) ( )
( ) ysh y C sh y ( )
( )
ych y
cos
xy
1
2
3
4
x y
where constants 1 , , C C C C are determined by relevant stress boundary conditions. For the test problem (Fig. 2), the boundary conditions can be represented in the form of symmetric expansion into a Fourier series: 2 3 4 ,
m x
0 m q A A 1
(16)
cos m
l
where the expansion coefficients are defined by the following expressions:
m a
2 sin q
1 cos a
m x
, qa A l
l
A q
dx
(17)
m
0
l
l
m
a
, C C C C in expressions for stresses (15):
With account of the boundary conditions, the constants 1 2 3 4 , ,
2 q sh h hch h ( ) ( )
C
1
2
(2 ) 2
sh h
h
a
cos
( ) (2 ) 2 sh h
q
2
C
(18)
4
2
c
sh h
a
cos
C C
0
2
3
where q- is determined by expression (16). The results of an analytical solution for middle line (y=0) on which only a normal stress takes place:
262
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