[UPDATE] Wing Design documentation

Description

Update of Wing Design documentation

docs/documentation/sizing/wing_design/basic-concepts.md

@@ -2,20 +2,20 @@
 
 Designing a wing for an aircraft is by far one of the most challenging tasks. This topic provides basic information for wings.
 
-If you are already familiar with the basic concepts, you can move on to the [Getting Started](getting-started.md).
-
+If you are already familiar with the basic concepts, you can move on to the [:octicons-arrow-right-16: Getting Started](getting-started.md).
 
 ### Available configurations
 Here you can find available wing build methods from the _wing\_design_ tool inside UNICADO.
+
 - _UNICADO is shipped natively with the cantilever wing method for a tube and wing configuration._
 - _A basic Blended Wing body method is planned!_
 
-<pre class='mermaid'>
+```mermaid
   graph LR;
     A[Wing Design]-->B[Tube and Wing];
     B-->C[Cantilever];
     A-->D[Blended Wing body]
-</pre>
+```
 
 !!! danger "Important"
     Since the documentation might be delayed to the development progress - this graph might not have all information yet.
@@ -37,45 +37,47 @@ Wing loading is the mass / weight of the aircraft distributed over its reference
 Understanding the wing geometry is crucial for designing an efficient wing. Below are key terms and their meanings:
 
 - Aspect Ratio (_AR_): The ratio of the wingspan to the average chord length
-  - _AR= b&sup2; / S_
-  - _b : Wingspan_
-  - _S : Wing reference area (projected area on ground from top view)_
-  - _High AR (e.g. gliders) &rarr; increased aerodynamic efficiency (higher drag) but slender and more flexible wing._
-  - _Low AR (e.g., fighter jets) &rarr; decreased aerodynmic efficiency and stiffer._
+    - _AR= b&sup2; / S_
+    - _b : Wingspan_
+    - _S : Wing reference area (projected area on ground from top view)_
+    - _High AR (e.g. gliders) &rarr; increased aerodynamic efficiency (higher drag) but slender and more flexible wing._
+    - _Low AR (e.g., fighter jets) &rarr; decreased aerodynmic efficiency and stiffer._
 
 - Taper Ratio (&lambda;): The ratio of the tip chord to the root chord.
-  - _&lambda;_ = _c_<sub>_tip_</sub> / _c_<sub>_root_</sub>
-  - _A taper ratio of one indicates a rectangular wing._
-  - _Reduced taper ratio can improve aerodynamic efficiency and reduce structural weight._
+    - _&lambda;_ = _c_<sub>_tip_</sub> / _c_<sub>_root_</sub>
+    - _A taper ratio of one indicates a rectangular wing._
+    - _Reduced taper ratio can improve aerodynamic efficiency and reduce structural weight._
 
 - Sweep Angle (&Phi;): The angle between the chord at a given position and a line perpendicular to the chord
-  - _Increased sweep leads to higher overall speeds due to reduction of the mach number normal to the leading edge_
-    - _backward sweep: increased aerodynamic load at the outer wing part &rarr; bad behaviour at high angle of attack (AoA)_
-    - _forward sweep: decreased aerodynamic load at the outer wing part but increased structural load due to wing torsion effects_
+    - _Increased sweep leads to higher overall speeds due to reduction of the mach number normal to the leading edge_
+        - _backward sweep: increased aerodynamic load at the outer wing part &rarr; bad behaviour at high angle of attack (AoA)_
+        - _forward sweep: decreased aerodynamic load at the outer wing part but increased structural load due to wing torsion effects_
 
 - Dihedral / Anhedral Angle (&nu;): Effects wing clearance and roll stability due to sideslip
-  - Common dihedral angle (positive) for low wing configuration
-  - Common anhedral angle (negative) for shoulder or high wing configurations
+    - Common dihedral angle (positive) for low wing configuration
+    - Common anhedral angle (negative) for shoulder or high wing configurations
 
 - Kink: Discontinuity in the wing trailing edge due to change in trailing edge sweep
-  - mostly occurs on aircraft from inner to outer wing (low configuration) which is affected by the engine and landing gear vice versa
+    - mostly occurs on aircraft from inner to outer wing (low configuration) which is affected by the engine and landing gear vice versa
 
 ### Airfoil selection
 An airfoil defines the cross-sectional shape of a wing. The key characteristics include:
 
 - Camber: Airfoil curvature
-  - _High camber  - generates more lift but comes with increased drag_
-  - _No camber (symmetrical) often used for aerobatic A/C_
-  - _Chord: Defines the length of the line from leading to trailing edge_
-  - _Thickness to Chord Ratio (t/c): maximum airfoil thickness in relation to its chord length_
-  - _affects lift, drag and wing cross section_
+    - _High camber  - generates more lift but comes with increased drag_
+    - _No camber (symmetrical) often used for aerobatic A/C_
+    - _Chord: Defines the length of the line from leading to trailing edge_
+    - _Thickness to Chord Ratio (t/c): maximum airfoil thickness in relation to its chord length_
+    - _affects lift, drag and wing cross section_
 
 
 ### Spar Placements
 Spars are the one of the main structural elements inside the wing to provide strength and rigidity
-  - _Has effects size of slats, flaps and integral tank size_
+
+- _Has effects size of slats, flaps and integral tank size_
 
 
 ### Winglet / Raked wingtip / Rakelet (not available yet):
 Additional aerodynamic component at the tip of the main wing section
+
 - _Used for induced drag reduction_