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ESI Special Topics, December 2007
Citing URL: http://www.esi-topics.com/erf/2007/december07-TayfunETezduyar.html

From •>>December 2007

Tayfun E. TezduyarTayfun E. Tezduyar answers a few questions about this month's fast moving front in the field of Engineering. The author has also sent along images of their work.


Engineering
Article: Computation of moving boundaries and interfaces and stabilization parameters
Authors: Tezduyar, TE
Journal: INT J NUMER METHOD FLUID, 43 (5): 555-575 OCT 20 2003
Addresses:
Rice Univ, MS 321,6100 Main St, Houston, TX 77005 USA.
Rice Univ, Houston, TX 77005 USA.


ST:  Why do you think your paper is highly cited?

This paper covers two interrelated topics that have attracted many researchers. Moving boundaries and interfaces include fluid-structure interactions, which have been very popular in recent years, and two-fluid flows, which have been equally popular. Determination of the stabilization parameters involved in the popular stabilized methods has also been attracting much attention because of its importance in the performance of the stabilized methods.

ST:  Does it describe a new discovery, methodology, or synthesis of knowledge?


“The numerical methods described in the paper are some of the core technologies we are using in computer modeling of the new parachutes to be used with NASA’s Orion space vehicle..”

The paper describes a number of new methods for the solution of flows with moving boundaries and interfaces, as well as new and systematic ways of determining the stabilization parameters.

ST:  Would you summarize the significance of your paper in layman’s terms?

The paper describes a number of new methods and ideas to make computer modeling of fluid mechanics and fluid-structure interaction problems more effective.

ST:  How did you become involved in this research and were any particular problems encountered along the way?

I have always been interested in the two topics covered by the paper, and the work presented in the paper was my way of pushing the front just a little bit more.

ST:  Where do you see your research leading in the future?

I look forward to increasing my research collaboration with many talented researchers who are also working on these two topics and increasing the scope and performance of the computer modeling techniques for fluid mechanics and fluid-structure interaction problems.

ST:  Are there any social or political implications for your research?

The numerical methods described in the paper are some of the core technologies we are using in computer modeling of the new parachutes to be used with NASA’s Orion space vehicle. These methods are also among the core technologies we are using in patient-specific computer modeling of arterial dynamics and blood flow, including the modeling of cerebral aneurysms.End

Tayfun E. Tezduyar, Ph.D.
James F. Barbour Professor in Mechanical Engineering
Mechanical Engineering and Materials Science
Rice University
Houston, TX, USA


A Closer Look...

A closer look... Below are images sent in by Tayfun E. Tezduyar which were obtained from computer modeling with core numerical technologies described in the cited paper.

Figure 1:

Figure 1: Patient-specific computer modeling of the arterial dynamics and blood flow for a middle cerebral artery segment with aneurysm. The arterial geometry is a close approximation to the computer tomography model from a 57 year-old male with cerebral aneurysm. The core numerical technologies are coming from the cited paper. For more information on this particular simulation, see T.E. Tezduyar, S. Sathe, M. Schwaab and B.S. Conklin, "Arterial Fluid Mechanics Modeling with the Stabilized Space-Time Fluid-Structure Interaction Technique", International Journal for Numerical Methods in Fluids, published online, October 2007, DOI: 10.1002/fld.1633.


Figure 2:

Figure 2: Patient-specific computer modeling of the arterial dynamics and blood flow for a bifurcating middle cerebral artery segment with aneurysm. The arterial geometry is a close approximation to the computer tomography model from a 59 year-old female with cerebral aneurysm. The core numerical technologies are coming from the cited paper. For more information on this particular simulation, see T.E. Tezduyar, S. Sathe, T. Cragin, B. Nanna, B.S. Conklin, J. Pausewang and M. Schwaab, "Modeling of Fluid-Structure Interactions with the Space-Time Finite Elements: Arterial Fluid Mechanics", International Journal for Numerical Methods in Fluids, 54 (2007) 901-922.


Figure 3:

Figure 3: Computer modeling of a ringsail parachute to be used with NASA Orion space vehicle. The figures show the parachute shape and flow field before and 6 seconds after the heat shield is dropped to decrease the landing speed. The core numerical technologies are coming from the cited paper. For more information on this particular simulation, see T.E. Tezduyar, S. Sathe, J. Pausewang, M. Schwaab, J. Crabtree and J. Christopher, "Air-Fabric Interaction Modeling with the Stabilized Space-Time FSI Technique", Proceedings of the Third Asian-Pacific Congress on Computational Mechanics, Kyoto, Japan, CD-ROM (2007).

     

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ESI Special Topics, December 2007
Citing URL: http://www.esi-topics.com/erf/2007/december07-TayfunETezduyar.html

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