Computational Mechanics Research and Support for Aerodynamics ...

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Energy Systems Division Argonne National Laboratory 9700 South Cass Avenue, Bldg. 362 Argonne, IL 60439-4815 www.anl.gov U.S. DEPARTMENT OF ENERGY Argonne National Laboratory is a U.S. Department of Energy laboratory managed by UChicago Argonne, LLC
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ANL/ESD/11-39 Computational Mechani
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ANL/ESD/11-39 Computational Mechani
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Computational Mechanics Research an
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3.3.4. Simplifying Assumptions ....
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Figure 2.22: Velocity distribution
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List of Tables Table 2.1: Boundary
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experiments at TFHRC continued. A m
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2. Computational Fluid Dynamics for
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( ) ( ) (2.8) where A 0, A 1, and n
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efine the rate function to improve
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The objective of this work is to de
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2.3.2. Mesh Refinement Study As det
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Table 2.2: Details of the various m
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indicating the surface averaged vel
Page 29 and 30: Figure 2.13: Line probes created at
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: Figure 3.32 Comparison of the initi
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