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from that of mesh 4 but close, and either would be adequate for engineering purposes. When the corrugated section is further refined with respect to the base in case of mesh 6, the path of the curve is initially as expected but contains an irregular ripple. The cause of this effect is currently unknown. Figure 2.12: Surface averaged velocity vs. length of the plane section (created at a trough) plot for meshes 4-6 2.3.3.2. Velocity Profile Variation with Mesh Refinement Line probes have been created along the flow section in the STAR-CCM+ software. In this particular case line probes have been created at a trough and a crest which are the regions of major interest. Each of the line probes created has 30 points on the line. The value of the Velocity magnitude of the flow is extracted at that particular point. Velocity profiles have been plotted using the line probes at a trough and a crest along the reduced barrel section. By taking a close look at the velocity profiles, it is possible to better analyze the nature of the flow. TRACC/TFHRC Y1Q3 Page 24
Figure 2.13: Line probes created at a trough and a crest along the flow field in the reduced barrel Figure 2.14: Velocity profiles of the different mesh cases with base size as 10mm plotted at a crest TRACC/TFHRC Y1Q3 Page 25
Page 1 and 2: ANL/ESD/11-39 Computational Mechani
Page 3 and 4: ANL/ESD/11-39 Computational Mechani
Page 5 and 6: Computational Mechanics Research an
Page 7 and 8: 3.3.4. Simplifying Assumptions ....
Page 9 and 10: Figure 2.22: Velocity distribution
Page 11 and 12: List of Tables Table 2.1: Boundary
Page 13 and 14: experiments at TFHRC continued. A m
Page 15 and 16: 2. Computational Fluid Dynamics for
Page 17 and 18: ( ) ( ) (2.8) where A 0, A 1, and n
Page 19 and 20: efine the rate function to improve
Page 21 and 22: The objective of this work is to de
Page 23 and 24: 2.3.2. Mesh Refinement Study As det
Page 25 and 26: Table 2.2: Details of the various m
Page 27: indicating the surface averaged vel
Page 31 and 32: In Figure 2.15 the velocity and the
Page 33 and 34: Mesh 1 Mesh 2 Mesh 3 Mesh 4 Mesh 5
Page 35 and 36: Figure 2.20: Dimensional details of
Page 37 and 38: Figure 2.22: Velocity distribution
Page 39 and 40: Figure 2.25: CFD velocity contour p
Page 41 and 42: Figure 2.27: CFD velocity contour p
Page 43 and 44: Conclusions for Comparison with Exp
Page 45 and 46: 3.1.1.1. Approach To date, an initi
Page 47 and 48: Figure 3.4: Sampling domain [3] A c
Page 49 and 50: present. In addition during the sum
Page 51 and 52: For each level, the figures below s
Page 53 and 54: 0.0 sec 0.5 sec 1.0 sec 1.5 sec 2.0
Page 59 and 60: 3.2.1. Vehicle Stability under High
Page 61 and 62: ̇ = steer angle These equations co
Page 63 and 64: ̈ With the success to the above an
Page 65 and 66: command. This requires the creation
Page 67 and 68: Figure 3.17: FEM Model of a Ford F-
Page 69 and 70: 3) Chen, F. and Chen, S., “Assess
Page 71 and 72: 75 50 25 Force (N) 0 -25 -50 -75 -1
Page 73 and 74: while the passive system has fixed
Page 75 and 76: the controllable EMSA. Simulations
Page 77 and 78: 4. Build a shell container with the
Page 79 and 80:
Figure 3.32 Comparison of the initi
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