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Merge pull request #601 from DLR-SL/develop
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merge develop into master for 3.1 release
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MarAlder authored Aug 26, 2019
2 parents b3b7fde + 82b97fa commit abaf240
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Showing 22 changed files with 44,222 additions and 62,282 deletions.
6 changes: 2 additions & 4 deletions development/release.md
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Expand Up @@ -15,11 +15,9 @@ The release process is grouped into the following steps:

## 1. Create documentation --> createDocumentation.bat

## 2. Create dummy file

## 3. Create libraries --> generateLibraries.bat
## 2. Create libraries --> generateLibraries.bat

Currently, CPACS is supported by TIXI and TIGL as interfaces to CPACS. Additionally, there is the possibility to create bindings for other languages as well. This becomes especially handy once users try to generate CPACS files. Within the CPACS release schedule two binding will be generated: Python and Java. The Python bindings are created using the generateDS library; Java bindings via JAXB, see the tools section. Both calls are listed in the generateLibraries batch file.

## 4. Upload files
## 3. Upload files
tbd
42 changes: 40 additions & 2 deletions documentation/Cpacs_doc_project.shfbproj
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Expand Up @@ -45,8 +45,8 @@
<MissingTags>Summary, Parameter, Returns, Remarks, AutoDocumentCtors, Namespace, TypeParameter</MissingTags>
<CopyrightHref>
</CopyrightHref>
<CopyrightText>%28c%29 2018 Deutsches Zentrum fuer Luft- und Raumfahrt e.V.</CopyrightText>
<FeedbackEMailAddress>jonas.jepsen%40dlr.de</FeedbackEMailAddress>
<CopyrightText>%28c%29 2019 Deutsches Zentrum fuer Luft- und Raumfahrt e.V.</CopyrightText>
<FeedbackEMailAddress>marko.alder%40dlr.de</FeedbackEMailAddress>
<FeedbackEMailLinkText>
</FeedbackEMailLinkText>
<HeaderText>
Expand Down Expand Up @@ -330,6 +330,44 @@
<AlternateText>paramam Sbot wing Ansys Lc</AlternateText>
</Image>
</ItemGroup>
<ItemGroup>
<Image Include="equations\stress_strain_anisotropicSolid.png">
<ImageId>stress_strain_anisotropicSolid</ImageId>
<AlternateText>stress_strain_anisotropicSolid</AlternateText>
</Image>
<Image Include="equations\stress_strain_anisotropicShell.png">
<ImageId>stress_strain_anisotropicShell</ImageId>
<AlternateText>stress_strain_anisotropicShell</AlternateText>
</Image>
<Image Include="equations\G_E_nu_relation.png">
<ImageId>G_E_nu_relation</ImageId>
<AlternateText>G= \frac{E}{2(1+\nu)}</AlternateText>
</Image>
<Image Include="equations\strain_stress_orthotropicSolid.png">
<ImageId>strain_stress_orthotropicSolid</ImageId>
<AlternateText>strain_stress_orthotropicSolid</AlternateText>
</Image>
<Image Include="equations\nu_E_othotropicMaterial.png">
<ImageId>nu_E_othotropicMaterial</ImageId>
<AlternateText>nu_E_othotropicMaterial</AlternateText>
</Image>
<Image Include="equations\strain_stress_orthotropicShell.png">
<ImageId>strain_stress_orthotropicShell</ImageId>
<AlternateText>strain_stress_orthotropicShell</AlternateText>
</Image>
<Image Include="equations\stress_strain_orthotropicShell.png">
<ImageId>stress_strain_orthotropicShell</ImageId>
<AlternateText>stress_strain_orthotropicShell</AlternateText>
</Image>
<Image Include="equations\Q_EngineeringConstants_orthotropicShell.png">
<ImageId>Q_EngineeringConstants_orthotropicShell</ImageId>
<AlternateText>Q_EngineeringConstants_orthotropicShell</AlternateText>
</Image>
<Image Include="material_coordinates.png">
<ImageId>material_coordinates</ImageId>
<AlternateText>material_coordinates</AlternateText>
</Image>
</ItemGroup>
<!-- Import the SHFB build targets -->
<Import Project="$(SHFBROOT)\SandcastleHelpFileBuilder.targets" />
</Project>
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Q_{11}=\frac{E_1}{1-\nu_{12}\nu_{21}} \; , \quad
Q_{22}=\frac{E_2}{1-\nu_{12}\nu_{21}} \; , \quad
\newline
Q_{12}=\frac{\nu_{12} E_2}{1-\nu_{12}\nu_{21}} = \frac{\nu_{21} E_1}{1-\nu_{12}\nu_{21}} \; , \quad
Q_{33}=G_{12}
Binary file added documentation/equations/nu_E_othotropicMaterial.png
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1 change: 1 addition & 0 deletions documentation/equations/nu_E_othotropicMaterial.tex
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\frac{\nu_{ij}}{E_i}=\frac{\nu_{ji}}{E_j}
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20 changes: 20 additions & 0 deletions documentation/equations/strain_stress_orthotropicShell.tex
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\begin{pmatrix}
\varepsilon_1 \\
\varepsilon_2 \\
\gamma_{12}
\end{pmatrix}

=

\begin{bmatrix}
\frac{1}{E_1} & -\frac{\nu_{21}}{E_2} & 0 \\
-\frac{\nu_{12}}{E_1}& \frac{1}{E_2} & 0 \\
0 & 0 & \frac{1}{G_{12}} \\

\end{bmatrix}

\begin{pmatrix}
\sigma_1 \\
\sigma_2 \\
\tau_{12}
\end{pmatrix}
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30 changes: 30 additions & 0 deletions documentation/equations/strain_stress_orthotropicSolid.tex
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\begin{pmatrix}
\varepsilon_1 \\
\varepsilon_2 \\
\varepsilon_3 \\
\gamma_{23} \\
\gamma_{31} \\
\gamma_{12}
\end{pmatrix}



=

\begin{bmatrix}
\frac{1}{E_1} & -\frac{\nu_{21}}{E_2} & -\frac{\nu_{31}}{E_3} & 0 & 0 & 0 \\
-\frac{\nu_{12}}{E_1}& \frac{1}{E_2} & -\frac{\nu_{32}}{E_3} & 0 & 0 & 0 \\
-\frac{\nu_{13}}{E_1}& -\frac{\nu_{23}}{E_2} & \frac{1}{E_3} & 0 & 0 & 0 \\
0 & 0 & 0 & \frac{1}{G_{23}} & 0 & 0 \\
0 & 0 & 0 & 0 & \frac{1}{G_{31}} & 0 \\
0 & 0 & 0 & 0 & 0 & \frac{1}{G_{12}} \\
\end{bmatrix}

\begin{pmatrix}
\sigma_1 \\
\sigma_2 \\
\sigma_3 \\
\tau_{23}\\
\tau_{31}\\
\tau_{12}
\end{pmatrix}
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30 changes: 30 additions & 0 deletions documentation/equations/stress_strain_anisotropicShell.tex
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\begin{pmatrix}
\sigma_1 \\
\sigma_2 \\
\tau_{12}
\end{pmatrix}

=

\begin{bmatrix}
Q_{11} & Q_{12} & Q_{13} \\
& Q_{22} & Q_{23} \\
\text{symm.} & & Q_{33}
\end{bmatrix}

\left(
\begin{pmatrix}
\varepsilon_1 \\
\varepsilon_2 \\
\gamma_{12}
\end{pmatrix}
-
\left( T - T_{\text{ref}} \right )

\begin{pmatrix}
\text{thermalExpansionCoeff}_1 \\
\text{thermalExpansionCoeff}_2 \\
\text{thermalExpansionCoeff}_{12}
\end{pmatrix}

\right )
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42 changes: 42 additions & 0 deletions documentation/equations/stress_strain_anisotropicSolid.tex
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\begin{pmatrix}
\sigma_1 \\
\sigma_2 \\
\sigma_3 \\
\tau_{23}\\
\tau_{31}\\
\tau_{12}
\end{pmatrix}

=

\begin{bmatrix}
C_{11} & C_{12} & C_{13} & C_{14} & C_{15} & C_{16} \\
& C_{22} & C_{23} & C_{24} & C_{25} & C_{26} \\
& & C_{33} & C_{34} & C_{35} & C_{36} \\
& & & C_{44} & C_{45} & C_{46} \\
& \text{symm.} & & & C_{55} & C_{56} \\
& & & & & C_{66}
\end{bmatrix}

\left(
\begin{pmatrix}
\varepsilon_1 \\
\varepsilon_2 \\
\varepsilon_3 \\
\gamma_{23} \\
\gamma_{31} \\
\gamma_{12}
\end{pmatrix}
-
\left( T - T_{\text{ref}} \right )

\begin{pmatrix}
\text{thermalExpansionCoeff}_1 \\
\text{thermalExpansionCoeff}_2 \\
\text{thermalExpansionCoeff}_3 \\
\text{thermalExpansionCoeff}_{23} \\
\text{thermalExpansionCoeff}_{31} \\
\text{thermalExpansionCoeff}_{12}
\end{pmatrix}

\right )
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33 changes: 33 additions & 0 deletions documentation/equations/stress_strain_orthotropicShell.tex
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@@ -0,0 +1,33 @@
\begin{pmatrix}
\sigma_1 \\
\sigma_2 \\
\tau_{12}
\end{pmatrix}

=

\begin{bmatrix}
Q_{11} & Q_{12} & 0 \\
Q_{12}& Q_{22} & 0 \\
0 & 0 & Q_{33} \\
\end{bmatrix}

\left(
\begin{pmatrix}
\varepsilon_1 \\
\varepsilon_2 \\
\gamma_{12}
\end{pmatrix}

-
\left( T - T_{\text{ref}} \right )

\begin{pmatrix}
\text{thermalExpansionCoeff}_1 \\
\text{thermalExpansionCoeff}_2 \\
0 \\

\end{pmatrix}


\right )
Binary file added documentation/material_coordinates.png
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