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From page 123...
... 123 A full-scale crash test was performed to validate the preliminary design guidelines and/or modify them as necessary. The finite element analysis using LS-DYNA was performed to help plan and predict the outcome of the TL-3 crash test.
From page 124...
... 124 • Modeling the 0.81 m (32 in.) high vertical barrier with explicit reinforcement details as shown in Figure 6.1 • Raising the wall height to reflect an MSE wall configuration composed of two rows of 1.52 m (5 ft)
From page 125...
... 125 B1B2B3B4B6 B5 Joint between Moment Slab (a) Three-dimensional view (b)
From page 126...
... 126 0 1000 2000 3000 4000 5000 6000 7000 0 0.1 0.2 0.3 0.4 0.5 W ei gh t ( kN )
From page 127...
... 127 6.2.1 Barrier Damage and Displacement The calculated impact force on the barrier was 248.21 kN (55.8 kips) at 0.0575 sec as shown in Figure 6.8.
From page 128...
... 128 6.2.2 Loads and Displacements in Reinforcement Strips The load–time histories for selected strips in the upper layer of reinforcement are presented in Figure 6.13(a)
From page 129...
... B3 B4 Figure 6.10. Damage to the back of the concrete barrier (0.1 sec)
From page 130...
... 130 0 0.5 1 1.5 2 Lo ad (k ips )
From page 131...
... 131 2.5 3 B4-A-3rd B4-C-3rd 0 0.5 1 1.5 2 Lo ad (k ips )
From page 132...
... 132 -0.06 -0.04 -0.02 0 0.02 0.04 0.06 0.08 0.1 0.12 D is pl ac em en t ( in)
From page 133...
... 6.3 TL-3 Crash Test 6.3.1 10 ft High MSE Wall Construction and Test Installation An overall layout of the 3.05 m (10 ft) high MSE wall test installation is shown in Figure 6.22.
From page 134...
... 3.05 m (10 ft) long precast barrier–coping sections were cast in place in three 9.14 m (30 ft)
From page 135...
... 135 Selected reinforcement strips in the MSE wall were instrumented with strain gages to capture the tensile forces transmitted into the reinforcement during the full-scale crash test. A total of 14 strain gages were used.
From page 136...
... 136 of reinforcement, and one strain gage was placed in the center of the panel between the two layers of reinforcement. An accelerometer was mounted behind and at the top of the barrier section immediately downstream of impact (which was shown in the simulation to experience the maximum load and displacement)
From page 137...
... 137 Figure 6.27. Vehicle before test.
From page 138...
... 138 yawed clockwise and came to rest 53.34 m (175 ft) downstream of impact and 1.83 m (6 ft)
From page 139...
... 139 front bumper, hood, grill, radiator and support, fan, left front fender, left front and rear doors, left and right exterior bed, rear bumper, and tailgate. The windshield sustained stress cracks at the left lower corner, which radiated upward toward the roof and center.
From page 140...
... 140 where Fi(t) = the impact force φ(t)
From page 141...
... 141 (a) Longitudinal deceleration (b)
From page 142...
... 142 (a) Acceleration (b)
From page 143...
... 143 the range of 1.5 to −1.5 g. Examination of the impact events helps explain the barrier acceleration–time history.
From page 144...
... contact. The dynamic displacement associated with the initial impact of the barrier was 21.3 mm (0.84 in.)
From page 145...
... 145 Table 6.3. Dynamic loads on the wall reinforcement.
From page 146...
... 146 TL-3 B5 B4 B3 2 6 7 13 12 11 1 7 5 8 8 9 1 3 1 5 3 4 -2 3 1 4 5 3 1 2 1 1 3 0 -1 2 4 2 1 4 1 1 2 1 0 1 1 1 1 0 2 0 Figure 6.43. Permanent deflection of barrier and panels (units: mm)
From page 147...
... 147 6.5 Comparison of Test and Simulation A comparison between the results of the TL-3 test and the numerical simulations was conducted to establish confidence in the simulation for use in the guideline development process. Because the numerical simulation was modeled prior to performing the TL-3 test, the differences between the TL-3 test and simulation are listed below.
From page 148...
... 148 (a) Simulation (b)
From page 149...
... 149 (a) Simulation (b)
From page 151...
... 151 Figure 6.49. Inertia deceleration force and impact force on the barrier.

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