From: hartmann Date: Mon, 1 Jul 2002 11:31:47 +0000 (+0000) Subject: . X-Git-Url: https://gitweb.dealii.org/cgi-bin/gitweb.cgi?a=commitdiff_plain;h=f7ff5cd1d09141569b997bbfb8c956564e2b3532;p=dealii-svn.git . git-svn-id: https://svn.dealii.org/trunk@6210 0785d39b-7218-0410-832d-ea1e28bc413d --- diff --git a/deal.II/doc/publications/2002/hartmann-1.bib b/deal.II/doc/publications/2002/hartmann-1.bib new file mode 100644 index 0000000000..4ff32c921f --- /dev/null +++ b/deal.II/doc/publications/2002/hartmann-1.bib @@ -0,0 +1,20 @@ + + + + + + +
+
+@PhdThesis{Har02,
+  author = 	 {Ralf Hartmann},
+  title = 	 {Adaptive Finite Element Methods for the
+                  Compressible Euler Equations},
+  school = 	 {University of Heidelberg},
+  year = 	 2002
+}
+
+
+
+
diff --git a/deal.II/doc/publications/2002/hh_hyp2002.bib b/deal.II/doc/publications/2002/hh_hyp2002.bib new file mode 100644 index 0000000000..f74643f155 --- /dev/null +++ b/deal.II/doc/publications/2002/hh_hyp2002.bib @@ -0,0 +1,21 @@ + + + + + + +
+
+@InProceedings{HH02a,
+  author = 	 {Ralf Hartmann and Paul Houston},
+  title = 	 {Goal-Oriented A Posteriori Error Estimation
+                  for Multiple Target Functionals},
+  booktitle = 	 {Hyperbolic problems: theory, numerics, applications:
+                 ninth international conference in Pasadena, California, 2002},
+  year = 	 2002,
+  note =	 {submitted},
+  publisher =	 {Springer},
+}
+
+
diff --git a/deal.II/doc/publications/2002/hh_hyp2002.html b/deal.II/doc/publications/2002/hh_hyp2002.html new file mode 100644 index 0000000000..27f503344d --- /dev/null +++ b/deal.II/doc/publications/2002/hh_hyp2002.html @@ -0,0 +1,45 @@ + + + + + + + + +

Abstract:

+ +

+ In many applications the quantities of interest are a series of + target functionals of the solution to the governing system of + partial differential equations rather than the solution itself. For + example, in the field of aerodynamics, examples include the drag and + lift coefficients of an airfoil immersed into a fluid, the pressure + difference between the leading and trailing edges of the airfoil and + point evaluations of the density or pressure on the profile of the + airfoil. While traditionally these quantities are measured in wind + tunnel experiments, nowadays these experiments are increasingly + replaced by numerical simulations aiming to predict these quantities + to a high level of accuracy. +
+ In a series of previous articles, we have developed the theory of + goal--oriented a posteriori error estimation for + discontinuous Galerkin methods applied to inviscid compressible + fluid flows. On the basis of Type I a posteriori bounds we + considered the design of adaptive finite element algorithms that are + capable of generating optimal meshes specifically tailored to the + efficient computation of a single target functional of + practical interest. The purpose of the current article is to extend + this earlier work to the case when several target + functionals of the solution need to be simultaneously approximated + to a given level of accuracy. +

+
+

+


+
+Ralf Hartmann +
2002-06-17 +
+ +