The BERSAFE finite element system

1974 ◽  
Vol 6 (1) ◽  
pp. 15-24 ◽  
Author(s):  
T.K. Hellen ◽  
S.J. Protheroe
1986 ◽  
Vol 108 (4) ◽  
pp. 669-673 ◽  
Author(s):  
J. D. Jones

The performance of a Stirling engine regenerator subjected to sinusoidal mass flow rate and pressure variation is analyzed. It is shown that cyclic variations in the temperature of the matrix due to its finite mass lead to an increase in the apparent regenerator effectiveness, but a decrease in engine power. Approximate closed-form expressions for both of these effects are deduced. The results of this analysis are compared with the predictions of a finite-element system model, and good agreement is found.


2016 ◽  
Vol 9 (10) ◽  
pp. 3803-3815 ◽  
Author(s):  
Gheorghe-Teodor Bercea ◽  
Andrew T. T. McRae ◽  
David A. Ham ◽  
Lawrence Mitchell ◽  
Florian Rathgeber ◽  
...  

Abstract. We present a generic algorithm for numbering and then efficiently iterating over the data values attached to an extruded mesh. An extruded mesh is formed by replicating an existing mesh, assumed to be unstructured, to form layers of prismatic cells. Applications of extruded meshes include, but are not limited to, the representation of three-dimensional high aspect ratio domains employed by geophysical finite element simulations. These meshes are structured in the extruded direction. The algorithm presented here exploits this structure to avoid the performance penalty traditionally associated with unstructured meshes. We evaluate the implementation of this algorithm in the Firedrake finite element system on a range of low compute intensity operations which constitute worst cases for data layout performance exploration. The experiments show that having structure along the extruded direction enables the cost of the indirect data accesses to be amortized after 10–20 layers as long as the underlying mesh is well ordered. We characterize the resulting spatial and temporal reuse in a representative set of both continuous-Galerkin and discontinuous-Galerkin discretizations. On meshes with realistic numbers of layers the performance achieved is between 70 and 90 % of a theoretical hardware-specific limit.


1985 ◽  
Vol 20 (1-3) ◽  
pp. 17-29 ◽  
Author(s):  
Daniel R. Rehak ◽  
Walid T. Keirouz ◽  
Chris T. Hendrickson ◽  
Zoltan J. Cendes

2021 ◽  
Vol 387 ◽  
pp. 114195
Author(s):  
Andres M. Aguirre-Mesa ◽  
Manuel J. Garcia ◽  
Mauricio Aristizabal ◽  
David Wagner ◽  
Daniel Ramirez-Tamayo ◽  
...  

2011 ◽  
Vol 130-134 ◽  
pp. 195-199
Author(s):  
Xue Ling Zhang ◽  
Ya Hui Hu ◽  
Shu Feng Chai

How to deal with the model is important in analyzing structure system with finite element method, because the rationality of model has direct relationship with veracity of simulation result. In this paper some simplify modeling methods are expatiated. And an approach is supposed that combine simplifying complex model and rigid-treating sub-component which make model more close to reality. In final, an instance of multi-type-element system structure is computed to prove the correctness of the method.


1982 ◽  
pp. 115-125 ◽  
Author(s):  
A. Combescure ◽  
A. Hoffmann ◽  
P. Pasquet

Author(s):  
A. Combescure ◽  
A. Hoffmann ◽  
P. Pasquet

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