iccsa-20-wind

git clone https://git.igankevich.com/iccsa-20-wind.git
Log | Files | Refs

commit 0d69cec6cdb15dcbd48b65a3d0693608091f9c2b
parent a6b5392aaf59a3f6542b668859fbf35636ef58c4
Author: Ivan Gankevich <i.gankevich@spbu.ru>
Date:   Sat, 14 Mar 2020 18:48:43 +0300

Update manifest.

Diffstat:
Makefile | 4++--
gnuplot/bench-aurora-laptop-openmp.dat | 8++++++++
guix/manifest.scm | 4++--
main.tex | 6+++++-
4 files changed, 17 insertions(+), 5 deletions(-)

diff --git a/Makefile b/Makefile @@ -26,11 +26,11 @@ build/$(SLIDES).pdf: slides.tex @-$(LATEXMK) $(FLAGS) -xelatex -f $< build/%.eps: build/%.svg - inkscape -z --export-type=eps --export-file=$@ $< + inkscape -z --export-eps=$@ $< build/inkscape/%.eps: graphics/inkscape/%.svg @mkdir -p build/inkscape - inkscape -z --export-type=eps --export-file=$@ $< + inkscape -z --export-eps=$@ $< build/gnuplot/%.svg: gnuplot/%.gnuplot @mkdir -p build/gnuplot diff --git a/gnuplot/bench-aurora-laptop-openmp.dat b/gnuplot/bench-aurora-laptop-openmp.dat @@ -0,0 +1,8 @@ +8 164323.5 +7 168880.916666667 +6 170619.583333333 +5 195834.333333333 +4 229678.916666667 +3 219791.666666667 +2 315572.666666667 +1 615750.75 diff --git a/guix/manifest.scm b/guix/manifest.scm @@ -1,6 +1,6 @@ -(use-package-modules tex textutils) +(use-package-modules tex textutils inkscape maths) (use-modules (stables packages texlive)) (packages->manifest - (list texlive texlive-beamertheme-saintpetersburg)) + (list texlive texlive-beamertheme-saintpetersburg inkscape gnuplot)) diff --git a/main.tex b/main.tex @@ -302,6 +302,10 @@ vector in cartesian coordinates). Then the solution is written as and reduces to general form of the solution for potential flow around a cylinder given in~\eqref{eq-solution-cylinder}. +\subsection{Ship roll angle and velocity} + +\subsection{Computational performance analysis} + \section{Discussion} Solution on the boundary \eqref{eq-solution-on-the-boundary} provides simple @@ -318,7 +322,7 @@ the solution for potential flow around a cylinder which makes reflected velocity term reach maximum value for the point on the boundary, and for the point near the boundary the solution includes reflected velocity vectors for each panel. We compared both solutions (see fig.~\ref{fig-verification}) for a -cylinder with \(R=27.4429\), and discovered that maximum root mean square error +cylinder with \(R=27.4429\), and discovered that maximum root square error between the two is less than 1\%. \begin{figure}