From fd1177dd454288101e85f53be04f9777714fdc25 Mon Sep 17 00:00:00 2001
From: tobi <tobias.weckenmann@tum.de>
Date: Fri, 21 Feb 2025 06:35:37 +0100
Subject: [PATCH] Adapts docu slightly
---
.../sizing/propulsion_design/overview.md | 20 +++++++++++--------
1 file changed, 12 insertions(+), 8 deletions(-)
diff --git a/docs/documentation/sizing/propulsion_design/overview.md b/docs/documentation/sizing/propulsion_design/overview.md
index 58c4741..2854f84 100644
--- a/docs/documentation/sizing/propulsion_design/overview.md
+++ b/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
--
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