Computational Mechanics Research and Support for Aerodynamics ...

More documents

Recommendations

Info

About Argonne National Laboratory Argonne is a U.S. Department of Energy laboratory managed by UChicago Argonne, LLC under contract DE-AC02-06CH11357. The Laboratory’s main facility is outside Chicago, at 9700 South Cass Avenue, Argonne, Illinois 60439. For information about Argonne and its pioneering science and technology programs, see www.anl.gov. Availability of This Report This report is available, at no cost, at http://www.osti.gov/bridge. It is also available on paper to the U.S. Department of Energy and its contractors, for a processing fee, from: U.S. Department of Energy Office of Scientific and Technical Information P.O. Box 62 Oak Ridge, TN 37831-0062 phone (865) 576-8401 fax (865) 576-5728 reports@adonis.osti.gov Disclaimer This report was prepared as an account of work sponsored by an agency of the United States Government. Neither the United States Government nor any agency thereof, nor UChicago Argonne, LLC, nor any of their employees or officers, makes any warranty, express or implied, or assumes any legal liability or responsibility for the accuracy, completeness, or usefulness of any information, apparatus, product, or process disclosed, or represents that its use would not infringe privately owned rights. Reference herein to any specific commercial product, process, or service by trade name, trademark, manufacturer, or otherwise, does not necessarily constitute or imply its endorsement, recommendation, or favoring by the United States Government or any agency thereof. The views and opinions of document authors expressed herein do not necessarily state or reflect those of the United States Government or any agency thereof, Argonne National Laboratory, or UChicago Argonne, LLC.
ANL/ESD/11-39 Computational Mechanics Research and Support for Aerodynamics and Hydraulics at TFHRC, Year 1 Quarter 3 Progress Report by S.A. Lottes, R.F. Kulak, and C. Bojanowski Transportation Research and Analysis Computing Center (TRACC) Energy Systems Division, Argonne National Laboratory August 2011
Page 1: 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 and 28: 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 55 and 56:
0.5 sec 1.0 sec 1.5 sec 2.0 sec 3.0
Page 57 and 58:
0.5 sec 1.0 sec 1.5 sec 2.0 sec 3.0
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
show all

Computational Mechanics Research and Support for Aerodynamics ...

Create successful ePaper yourself

Delete template?

Save as template?