PSI - Issue 28
A.M. Bragov et al. / Procedia Structural Integrity 28 (2020) 2174–2180 Author name / Structural Integrity Procedia 00 (2019) 000–000
2176
3
From the one-dimensional theory of propagation of elastic waves in semi-infinite bars, it is known that the deformation in the wave (t) is related to the mass velocity dU/dt by a simple relation: ( ) 1 t dU C dt , (1) where the displacement U(t) of particles in the wave:
( ) t U t C t dt . ( )
(2)
0
The scheme of specimen loading in the SHPB set-up is shown in figure 1. Based on formula (2), it can record the movement of the ends of the bars 1 and 2 adjacent to the specimen. The movement of the left end face U 1 (t) is the sum of the movement U I 1 (t) caused by the propagation of the impulse ε I (t) and the movement U R 1 (t) caused by the propagation of the impulse ε R (t) : 1 0 0 0 ( ) ( ) ( ) ( ) ( ) t t t I R I R U t C t dt C t dt C t t dt . (3) When writing formulas for compressive pulses (incident I (t) and transmitted T (t) ), for which the particle mass velocity vector coincides with the direction of wave propagation, a plus sign is assigned. For the reflected tensile pulse R (t) , the vectors of the particle mass velocity and the wave propagation velocity are oppositely directed and, when calculating the displacements, the reflected momentum must be taken with a minus sign. The movement of the right end face U 2 (t) is caused by the propagation of the impulse T (t) :
2 t T U t C t dt . ( ) ( )
(4)
0
The average engineering strain of the specimen of length L 0 will be equal to:
( ) U t U t ( )
(5)
( ) t
s
1
2
L
0
or, if it is expressed through impulses in the bars:
t
C t
I
R
T
.
(6)
( ) t
( )
( ) t ( )
t dt
s
L
0 0
dt t d s s / ( ) :
Hence, the strain rate of the specimen
I C t
.
(7)
( )
( )
( ) t R
( ) t
T
s t
L
0
To find stress in the specimen, the forces at its ends should be considered. The force at the left end face Р 1 (t) is the sum of the compressive force P I 1 (t) caused by the impulse I (t) and the force P R 1 (t) caused by the impulse R (t) , and
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