Adapts docu slightly

docs/documentation/sizing/propulsion_design/overview.md

@@ -124,11 +124,15 @@ The detailed description of the engine library can be found [here](../../../libr
 
 The underlying principle is the scaling of the mass flow with constant velocities. The following scaling is done using the scale factor (SF):  
 
-- **Thrust:** Linear  
-- **Fuel Flow:** Linear → TSFC remains constant  
-- **Diameter:** \( SF^{0.5} \)  
-- **Weight:** \( SF^{1.1} \)  
-- **Length:** \( SF^{0.4} \)  
-- **LTO Fuel Flow:** Linear
-- **LTO Emissions:** Constant
-
+Scaled Value = Base Value * \( SF^{X} \)  
+
+- **Thrust:**       X=1  
+- **Fuel Flow:**    X=1 → TSFC remains constant  
+- **Diameter:**     X=0.5 
+- **Weight:**       X=1.1  
+- **Length:**       X=0.4 
+- **LTO Fuel Flow:** X=1
+- **LTO Emissions:** 0
+- **Mass Flow:**    X=1
+- **Max bleed:**    X=1
+- **Max shaft offtake:** X=1 
\ No newline at end of file