From fa8855c97e94f723e749a33b94fdd63834afdd56 Mon Sep 17 00:00:00 2001
From: Thomas Lambert <t.lambert@uliege.be>
Date: Mon, 19 Dec 2022 11:30:53 +0100
Subject: [PATCH] style: minor symbol changes
---
contents/tech-solvers.tex | 4 ++--
contents/user-input.tex | 5 ++++-
rotare-bib.bib | 1 -
style/symbols.sty | 6 ++++--
4 files changed, 10 insertions(+), 6 deletions(-)
diff --git a/contents/tech-solvers.tex b/contents/tech-solvers.tex
index 86dfa14..5f64f12 100644
--- a/contents/tech-solvers.tex
+++ b/contents/tech-solvers.tex
@@ -213,14 +213,14 @@ then given by:
\end{equation}
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
direction as:
\begin{equation}
\label{eq:tech:solvers:mom:thrust}
\begin{split}
d\thrust & = \mFlow (\vAx[d] - \vAx[u]) \\
- & = \mFlow \vSlip \\
+ & = \mFlow \vSlipAx \\
& = \mFlow (2\viAx) \\
& = 4\pi \dens (\vAx + \viAx) \viAx \radA \dy
\end{split}
diff --git a/contents/user-input.tex b/contents/user-input.tex
index a52c6c8..8d1de4a 100644
--- a/contents/user-input.tex
+++ b/contents/user-input.tex
@@ -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
(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
Chapter~\ref{chap:tech:solvers}.
+ \textit{It is possible to provide a cell array with multiple solvers. Rotare
+ will then loop for all solvers.}
}
diff --git a/rotare-bib.bib b/rotare-bib.bib
index e72ca7e..6bc53d7 100644
--- a/rotare-bib.bib
+++ b/rotare-bib.bib
@@ -23,4 +23,3 @@
location = {{Fort Worth, Texas, USA}},
keywords = {\#nosource,helicopters,IMPORTANT,methods/BEMT,rotors}
}
-
diff --git a/style/symbols.sty b/style/symbols.sty
index 0a2cdfb..88c4ff6 100644
--- a/style/symbols.sty
+++ b/style/symbols.sty
@@ -46,11 +46,13 @@
% Induced velocities
\newcommand{\viAx}{\ensuremath{v_{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]{\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
\newcommand{\axFact}{\ensuremath{a}}
--
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