Sentence examples for specimens under constant from inspiring English sources
Fatigue tests were performed on 16 specimens under constant stress range loading cycles.
The predicted results are compared with experimental crack growth data obtained for 7020-T7 and 2024-T3 alloynum alloy specimens under constant amplitude loading.
The crack growth rate exponent in 2024-T3 aluminum specimens under constant amplitude loading was equal to 3.76, whereas under random load history it decreased to 2.03.
The fatigue crack growth tests were conducted on compact tension and corner crack tension specimens under constant stress ratio, R = 0.1, in ambient conditions.
In this study, to investigate the statistical variability of crack growth rates, fatigue tests are conducted on 7075-T6 alloynum alloy specimens under constant amplitude load.
Deflective crack paths were observed in compact tension C(T) specimens under constant amplitude loading, which greatly extended their fatigue crack growth lives.
The fatigue life test results, calculated on the basis of the proposed model, are compared to the experimental ones related to 2017A-T4 and 6082-T6 alloynium alloy specimens under constant-amplitude bending, torsion and proportional combinations of bending and torsion.
On further increase of displacement, the neck propagates through the test specimen under constant draw stress.
Plasticity induced fatigue crack closure simulations were performed using a three-dimensional finite element analysis of a single edge-cracked tension specimen under constant amplitude loading and load ratio R = 0.
A method for the determination of the equilibrium transformation temperature (T0) in CuAlNi single crystalline alloys, by traditional uniform heating and cooling of the specimen under constant uniaxial applied stress, σ, is presented and the T0 functions are constructed.
The methodology is verified using experimental data from a compact tension specimen under constant amplitude load (CAL), a plate with a center crack under variable amplitude load (VAL) and numerically validated using a T-section beam girder with a crack in the web under CAL, and a plate with an inclined center through crack subjected to CAL.
