Blending Functions for Hermite Interpolation by Beta-Function B-Splines on Triangulations

Author(s):  
Børre Bang ◽  
Lubomir T. Dechevsky ◽  
Arne Lakså ◽  
Peter Zanaty
1989 ◽  
Vol 6 (2) ◽  
pp. 177-179 ◽  
Author(s):  
Mark S. Mummy

1990 ◽  
Vol 7 (3) ◽  
pp. 136-144 ◽  
Author(s):  
J.J.S.P. Cabral ◽  
L.C. Wrobel ◽  
C.A. Brebbia
Keyword(s):  

1991 ◽  
Vol 8 (6) ◽  
pp. 439-441 ◽  
Author(s):  
Hans-Peter Seidel

2019 ◽  
Vol 626 ◽  
pp. A108
Author(s):  
V. A. Baturin ◽  
W. Däppen ◽  
A. V. Oreshina ◽  
S. V. Ayukov ◽  
A. B. Gorshkov

Aims. We use Hermite splines to interpolate pressure and its derivatives simultaneously, thereby preserving mathematical relations between the derivatives. The method therefore guarantees that thermodynamic identities are obeyed even between mesh points. In addition, our method enables an estimation of the precision of the interpolation by comparing the Hermite-spline results with those of frequent cubic (B-) spline interpolation. Methods. We have interpolated pressure as a function of temperature and density with quintic Hermite 2D-splines. The Hermite interpolation requires knowledge of pressure and its first and second derivatives at every mesh point. To obtain the partial derivatives at the mesh points, we used tabulated values if given or else thermodynamic equalities, or, if not available, values obtained by differentiating B-splines. Results. The results were obtained with the grid of the SAHA-S equation-of-state (EOS) tables. The maximum lgP difference lies in the range from 10−9 to 10−4, and Γ1 difference varies from 10−9 to 10−3. Specifically, for the points of a solar model, the maximum differences are one order of magnitude smaller than the aforementioned values. The poorest precision is found in the dissociation and ionization regions, occurring at T ∼ 1.5 × 103−105 K. The best precision is achieved at higher temperatures, T >  105 K. To discuss the significance of the interpolation errors we compare them with the corresponding difference between two different equation-of-state formalisms, SAHA-S and OPAL 2005. We find that the interpolation errors of the pressure are a few orders of magnitude less than the differences from between the physical formalisms, which is particularly true for the solar-model points.


2014 ◽  
Vol 2014 ◽  
pp. 1-9 ◽  
Author(s):  
Christopher Provatidis

We compare contemporary practices of global approximation using cubic B-splines in conjunction with double multiplicity of inner knots (C1-continuous) with older ideas of utilizing local Hermite interpolation of third degree. The study is conducted within the context of the Galerkin-Ritz formulation, which forms the background of the finite element structural analysis. Numerical results, concerning static and eigenvalue analysis of rectangular elastic structures in plane stress conditions, show that both interpolations lead to identical results, a finding that supports the view that they are mathematically equivalent.


Author(s):  
Martin Ta¨ndl ◽  
Andre´s Kecskeme´thy

The article presents an object-oriented framework for representing guided spatial motion in multibody systems. In this setting, the spatial track is regarded as a kinetostatic transmission element transmitting motion and forces as in a generic joint. For vector decompositions along the path, three different parametrizations (Frenet and Darboux frames, respectively, as well as the ODE generation proposed by Bishop) are analyzed. It is shown that for the Frenet frame parametrization, it is possible to avoid singularities at the points of inflection by a special blending technique. Track geometry is globally smoothed up to fifth order using B-Splines and Dierckx optimization routines, thus allowing for non-jerky acceleration layout. Roll-angle or banking information is additionally generated by globally smooth splines, thus also allowing for non-jerky rotations along the track. Local editing is made possible through the use of exponential blending functions. The result is a robust and easily applicable software that can be integrated in general environments. All concepts have been implemented in a multibody simulation program and tested within an industrial application of roller coaster design.


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