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Verified Commit fa8855c9 authored by Thomas Lambert's avatar Thomas Lambert :helicopter:
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style: minor symbol changes

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...@@ -213,14 +213,14 @@ then given by: ...@@ -213,14 +213,14 @@ then given by:
\end{equation} \end{equation}
Furthermore, it can be showed that axial induced velocity at the disk is equal Furthermore, it can be showed that axial induced velocity at the disk is equal
to half the slipstream velocity in the far wake: $\viAx = \frac{\vSlip}{2}$. to half the slipstream velocity in the far wake: $\viAx = \frac{\vSlipAx}{2}$.
The thrust can then be expressed using the momentum balance in the axial The thrust can then be expressed using the momentum balance in the axial
direction as: direction as:
\begin{equation} \begin{equation}
\label{eq:tech:solvers:mom:thrust} \label{eq:tech:solvers:mom:thrust}
\begin{split} \begin{split}
d\thrust & = \mFlow (\vAx[d] - \vAx[u]) \\ d\thrust & = \mFlow (\vAx[d] - \vAx[u]) \\
& = \mFlow \vSlip \\ & = \mFlow \vSlipAx \\
& = \mFlow (2\viAx) \\ & = \mFlow (2\viAx) \\
& = 4\pi \dens (\vAx + \viAx) \viAx \radA \dy & = 4\pi \dens (\vAx + \viAx) \viAx \radA \dy
\end{split} \end{split}
......
...@@ -181,9 +181,12 @@ The structure \lstmat{Mod} contains the parameters for the solvers and the ...@@ -181,9 +181,12 @@ The structure \lstmat{Mod} contains the parameters for the solvers and the
extension and corrections to apply. It also specifies the numerical limits extension and corrections to apply. It also specifies the numerical limits
(number of iterations, precision, etc.). (number of iterations, precision, etc.).
\describeOption{Mod.solver}{}{\lst{'leishman', 'prop', 'turbine', 'stahlhut'}}{ \describeOption{Mod.solvers}{}{\lst{'leishman', 'prop', 'turbine', 'stahlhut',
'all'}}{
Type of solver to use. The solvers are described in length in Type of solver to use. The solvers are described in length in
Chapter~\ref{chap:tech:solvers}. Chapter~\ref{chap:tech:solvers}.
\textit{It is possible to provide a cell array with multiple solvers. Rotare
will then loop for all solvers.}
} }
......
...@@ -23,4 +23,3 @@ ...@@ -23,4 +23,3 @@
location = {{Fort Worth, Texas, USA}}, location = {{Fort Worth, Texas, USA}},
keywords = {\#nosource,helicopters,IMPORTANT,methods/BEMT,rotors} keywords = {\#nosource,helicopters,IMPORTANT,methods/BEMT,rotors}
} }
...@@ -46,11 +46,13 @@ ...@@ -46,11 +46,13 @@
% Induced velocities % Induced velocities
\newcommand{\viAx}{\ensuremath{v_{i}}} \newcommand{\viAx}{\ensuremath{v_{i}}}
\newcommand{\viTg}{\ensuremath{u_{i}}} \newcommand{\viTg}{\ensuremath{u_{i}}}
\newcommand{\vSlip}{\ensuremath{w}} \newcommand{\vSlipAx}{\ensuremath{v_w}}
\newcommand{\vSlipTg}{\ensuremath{u_w}}
\nomenclature[A]{\viAx}{Induced axial velocity\nomunit{\m\per\s}} \nomenclature[A]{\viAx}{Induced axial velocity\nomunit{\m\per\s}}
\nomenclature[A]{\viTg}{Induced tangential velocity\nomunit{\m\per\s}} \nomenclature[A]{\viTg}{Induced tangential velocity\nomunit{\m\per\s}}
\nomenclature[A]{\vSlip}{Slipsteam velocity in the far wake\nomunit{\m\per\s}} \nomenclature[A]{\vSlipAx}{Axial velocity in the far wake\nomunit{\m\per\s}}
\nomenclature[A]{\vSlipTg}{Tangential velocity in the far wake\nomunit{\m\per\s}}
% Induction factors % Induction factors
\newcommand{\axFact}{\ensuremath{a}} \newcommand{\axFact}{\ensuremath{a}}
......
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