2005
DOI: 10.1088/1742-6596/16/1/067
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Interoperable geometry and mesh components for SciDAC applications

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Cited by 6 publications
(7 citation statements)
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“…The assumption that the mesh boundary vertex coordinates of M d are known does not apply to many practical problems and must be dealt with; for the purpose of the present paper, these assumptions are made in order to focus on the problem of properly updating the interior vertex coordinates. A preliminary stab at the boundary problem is described in [7]. It is further assumed that boundary vertex positions are fixed in the optimization of the TMP objective function.…”
Section: Brief Overview Of the Target Paradigmmentioning
confidence: 99%
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“…The assumption that the mesh boundary vertex coordinates of M d are known does not apply to many practical problems and must be dealt with; for the purpose of the present paper, these assumptions are made in order to focus on the problem of properly updating the interior vertex coordinates. A preliminary stab at the boundary problem is described in [7]. It is further assumed that boundary vertex positions are fixed in the optimization of the TMP objective function.…”
Section: Brief Overview Of the Target Paradigmmentioning
confidence: 99%
“…The case d = 3 (three dimensions) was used with success in [7,9]. The case p = 1 was used for all of the examples.…”
Section: Numerical Examplesmentioning
confidence: 99%
“…This endeavor will far exceed the single CPU memory limitation of existing meshing software. A parallel meshing capability based on solid model has been developed together with U of Wisconsin and Sandia [10] that makes use of the CHACO graph library to partition the geometry into subdomains and then distribute them onto different processors. Figure 5 demonstrates the test case for a simplified ILC cavity with four sub-domains showing the efficacy of the method.…”
Section: Parallel Meshingmentioning
confidence: 99%
“…With the reduced gradient method, the optimality conditions consist of three parts: state equations, adjoint equations, and design equations. Researchers from TOPS are developing the optimization method [4] while those from TSTT are working on mesh movement and design variables computations [5]. SLAC is solving the state equations and the adjoint equations plus integrating all three components to develop a parallel capability.…”
Section: Achievement In Shape Optimizationmentioning
confidence: 99%