fix(fig): use correct symbols

figures/schematics/bladeElement.pdf_tex

-%% Creator: Inkscape 1.2.1 (9c6d41e4, 2022-07-14), www.inkscape.org
+%% Creator: Inkscape 1.2.1 (9c6d41e410, 2022-07-14, custom), www.inkscape.org
 %% PDF/EPS/PS + LaTeX output extension by Johan Engelen, 2010
 %% Accompanies image file 'bladeElement.pdf' (pdf, eps, ps)
 %%
@@ -38,7 +38,7 @@
   \newcommand*\fsize{\dimexpr\f@size pt\relax}%
   \newcommand*\lineheight[1]{\fontsize{\fsize}{#1\fsize}\selectfont}%
   \ifx\svgwidth\undefined%
-    \setlength{\unitlength}{542.2889609bp}%
+    \setlength{\unitlength}{576.58945692bp}%
     \ifx\svgscale\undefined%
       \relax%
     \else%
@@ -50,24 +50,27 @@
   \global\let\svgwidth\undefined%
   \global\let\svgscale\undefined%
   \makeatother%
-  \begin{picture}(1,0.58275999)%
+  \begin{picture}(1,0.61249781)%
     \lineheight{1}%
     \setlength\tabcolsep{0pt}%
     \put(0,0){\includegraphics[width=\unitlength,page=1]{bladeElement.pdf}}%
-    \put(0.17773997,0.13659041){\color[rgb]{0,0.36078431,0.6627451}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$V_A$\end{tabular}}}}%
-    \put(0.57463858,0.00716426){\color[rgb]{0,0.36078431,0.6627451}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$V_T$\end{tabular}}}}%
-    \put(0.57120019,0.16546396){\color[rgb]{0.35686275,0.14509804,0.49019608}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$V_R$\end{tabular}}}}%
+    \put(0.90576601,0.52395294){\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$\xtpp$\end{tabular}}}}%
+    \put(0.80690897,0.59159205){\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$\ztpp$\end{tabular}}}}%
     \put(0,0){\includegraphics[width=\unitlength,page=2]{bladeElement.pdf}}%
-    \put(0.67039662,0.24668755){\color[rgb]{0.90196078,0.17647059,0.19215686}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$dD$\end{tabular}}}}%
-    \put(0.62251979,0.55151152){\color[rgb]{0.90196078,0.17647059,0.19215686}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$dL$\end{tabular}}}}%
-    \put(0.74458349,0.52010309){\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$dR$\end{tabular}}}}%
+    \put(0.17497099,0.12923546){\color[rgb]{0,0.36078431,0.6627451}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$\vAx$\end{tabular}}}}%
+    \put(0.54045414,0.00750869){\color[rgb]{0,0.36078431,0.6627451}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$\vTg$\end{tabular}}}}%
+    \put(0.53722029,0.15639137){\color[rgb]{0.35686275,0.14509804,0.49019608}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$\vRel$\end{tabular}}}}%
     \put(0,0){\includegraphics[width=\unitlength,page=3]{bladeElement.pdf}}%
-    \put(0.52053127,0.51457098){\color[rgb]{0,0.43921569,0.49803922}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$dT$\end{tabular}}}}%
-    \put(0.74721248,0.2861535){\color[rgb]{0,0.43921569,0.49803922}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$dQ$\end{tabular}}}}%
+    \put(0.63051566,0.23278308){\color[rgb]{0.90196078,0.17647059,0.19215686}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$d\drag$\end{tabular}}}}%
+    \put(0.58548697,0.5194735){\color[rgb]{0.90196078,0.17647059,0.19215686}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$d\lift$\end{tabular}}}}%
+    \put(0.70028926,0.48993352){\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$dR$\end{tabular}}}}%
     \put(0,0){\includegraphics[width=\unitlength,page=4]{bladeElement.pdf}}%
-    \put(0.03303235,0.33264461){\color[rgb]{0.94117647,0.49803922,0.23529412}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$\beta$\\\end{tabular}}}}%
-    \put(0.29791669,0.1246871){\color[rgb]{0.94117647,0.49803922,0.23529412}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$\phi$\end{tabular}}}}%
-    \put(0.31858815,0.30648841){\color[rgb]{0.94117647,0.49803922,0.23529412}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$\alpha$\end{tabular}}}}%
-    \put(0.23154778,0.48713236){\color[rgb]{0.94117647,0.49803922,0.23529412}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$\alpha_0$\end{tabular}}}}%
+    \put(0.48176119,0.4847305){\color[rgb]{0,0.43921569,0.49803922}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$d\fZ$\end{tabular}}}}%
+    \put(0.70276186,0.26990126){\color[rgb]{0,0.43921569,0.49803922}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$d\fX$\end{tabular}}}}%
+    \put(0,0){\includegraphics[width=\unitlength,page=5]{bladeElement.pdf}}%
+    \put(0.03106731,0.31362667){\color[rgb]{0.94117647,0.49803922,0.23529412}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$\pitch$\\\end{tabular}}}}%
+    \put(0.28019404,0.11804027){\color[rgb]{0.94117647,0.49803922,0.23529412}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$\aInfl$\end{tabular}}}}%
+    \put(0.29963579,0.28902648){\color[rgb]{0.94117647,0.49803922,0.23529412}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$\aoa$\end{tabular}}}}%
+    \put(0.21777333,0.45892417){\color[rgb]{0.94117647,0.49803922,0.23529412}\makebox(0,0)[lt]{\lineheight{1.25}\smash{\begin{tabular}[t]{l}$\aoa_0$\end{tabular}}}}%
   \end{picture}%
 \endgroup%

style/symbols.sty

@@ -61,7 +61,9 @@
 
 % Other velocities
 \newcommand{\angVel}{\ensuremath{\Omega}}
+\newcommand{\rpsVel}{\ensuremath{n}}
 \nomenclature[G]{\angVel}{Angular velocity\nomunit{\per\s}}
+\nomenclature[A]{\rpsVel}{Angular velocity\nomunit{\per\s}}
 
 % Ratios
 \newcommand{\infRat}{\ensuremath{\lambda}}
@@ -83,7 +85,7 @@
 \newcommand{\pitch}{\ensuremath{\beta}}
 \newcommand{\aoaR}{\ensuremath{\zeta}}
 \newcommand{\azim}{\ensuremath{\psi}}
-\newcommand{\aInd}{\ensuremath{\phi}}
+\newcommand{\aInfl}{\ensuremath{\phi}}
 
 \nomenclature[G]{\aoa}{Angle of attack\nomunit{}}
 \nomenclature[G]{\twist}{Twist angle (stagger for propellers)\nomunit{}}
@@ -92,21 +94,23 @@
 \nomenclature[G]{\pitch}{Pitch angle\nomunit{}}
 \nomenclature[G]{\aoaR}{Rotor angle of attack\nomunit{}}
 \nomenclature[G]{\azim}{Azimuthal angle\nomunit{}}
-\nomenclature[G]{\aInd}{Induced angle\nomunit{}}
+\nomenclature[G]{\aInfl}{Induced angle\nomunit{}}
 
 % --- Lengths ------------------------------------------------------------------
 
 % Lengths
 \newcommand{\chord}{\ensuremath{c}}
 \newcommand{\radius}{\ensuremath{R}}
-\newcommand{\radR}{\ensuremath{r}}
+\newcommand{\diam}{\ensuremath{D}}
 \newcommand{\radA}{\ensuremath{y}}
 \newcommand{\dy}{\ensuremath{dy}}
+\newcommand{\radR}{\ensuremath{r}}
 
 \nomenclature[A]{\chord}{Rotor chord\nomunit{\m}}
 \nomenclature[A]{\radius}{Rotor radius\nomunit{\m}}
-\nomenclature[A]{\radR}{Nondimensional radial position\nomunit{-}}
+\nomenclature[A]{\diam}{Rotor diameter\nomunit{\m}}
 \nomenclature[A]{\radA}{Absolute radial position\nomunit{\m}}
+\nomenclature[A]{\radR}{Nondimensional radial position, $\frac{\radA}{\radius}$\nomunit{-}}
 
 % Surfaces
 \newcommand{\area}{\ensuremath{A}}
@@ -135,6 +139,8 @@
 \newcommand{\nBlades}{\ensuremath{N_b}}
 \nomenclature[A]{\nBlades}{Number of blades\nomunit{-}}
 
+\newcommand{\prandtl}{\ensuremath{F}}
+\nomenclature[A]{\prandtl}{Prandtl's tip-loss factor\nomunit{-}}
 
 % --- Forces, torques, powers, etc ---------------------------------------------
 
@@ -144,10 +150,11 @@
 \newcommand{\thrust}{\ensuremath{\mathcal{T}}} % Thrust
 \newcommand{\torque}{\ensuremath{\mathcal{Q}}} % Torque
 \newcommand{\power}{\ensuremath{\mathcal{P}}} % Power
-\newcommand{\ForceX}{\ensuremath{F_x}} % Rotor force along X_TPP-axis
-\newcommand{\ForceY}{\ensuremath{F_y}} % Rotor force along Y_TPP-axis
-\newcommand{\MomX}{\ensuremath{M_x}} % Rotor moment along X_TPP-axis
-\newcommand{\MomY}{\ensuremath{M_y}} % Rotor moment along Y_TPP-axis
+\newcommand{\fX}{\ensuremath{F_x}} % Rotor force along X_TPP-axis
+\newcommand{\fY}{\ensuremath{F_y}} % Rotor force along Y_TPP-axis
+\newcommand{\fZ}{\ensuremath{F_z}} % Rotor force along Z_TPP-axis
+\newcommand{\mX}{\ensuremath{M_x}} % Rotor moment along X_TPP-axis
+\newcommand{\mY}{\ensuremath{M_y}} % Rotor moment along Y_TPP-axis
 
 \nomenclature[A]{\lift}{Lift\nomunit{\N}}
 \nomenclature[A]{\drag}{Drag\nomunit{\N}}
@@ -163,10 +170,10 @@
 \newcommand{\cThrust}{\ensuremath{C_{\thrust}}} % Thrust coefficient
 \newcommand{\cTorque}{\ensuremath{C_{\torque}}} % Torque coefficient
 \newcommand{\cPower}{\ensuremath{C_{\power}}} % Power coefficient
-\newcommand{\cForceX}{\ensuremath{C_{F_x}}} % Longitudinal force coefficient
-\newcommand{\cForceY}{\ensuremath{C_{F_y}}} % Lateral side force coefficient
-\newcommand{\cMomX}{\ensuremath{C_{M_x}}} % Rolling moment coefficient
-\newcommand{\cMomY}{\ensuremath{C_{M_y}}} % Pitching moment coefficient
+\newcommand{\cfX}{\ensuremath{C_{F_x}}} % Longitudinal force coefficient
+\newcommand{\cfY}{\ensuremath{C_{F_y}}} % Lateral side force coefficient
+\newcommand{\cmX}{\ensuremath{C_{M_x}}} % Rolling moment coefficient
+\newcommand{\cmY}{\ensuremath{C_{M_y}}} % Pitching moment coefficient
 
 \nomenclature[A]{\cLift}{Lift coefficient\nomunit{-}}
 \nomenclature[A]{\cLiftSlope}{Lift curve slope\nomunit{-}}