From bfffb4aa9cc6684629413dc4e61a7df23a75e543 Mon Sep 17 00:00:00 2001
From: Johannes Schneider <johannes.schneider@ifb.uni-stuttgart.de>
Date: Mon, 10 Feb 2025 08:16:21 +0100
Subject: [PATCH] Apply 1 suggestion(s) to 1 file(s)
Co-authored-by: Ellen Seabrooke <ellen.seabrooke@ifb.uni-stuttgart.de>
---
docs/documentation/sizing/initial_sizing/initialSizing.md | 2 +-
1 file changed, 1 insertion(+), 1 deletion(-)
diff --git a/docs/documentation/sizing/initial_sizing/initialSizing.md b/docs/documentation/sizing/initial_sizing/initialSizing.md
index 101b0ac..d86785b 100644
--- a/docs/documentation/sizing/initial_sizing/initialSizing.md
+++ b/docs/documentation/sizing/initial_sizing/initialSizing.md
@@ -45,7 +45,7 @@ For the determination the following parameters are necessary:
1) acXML:
- Design range [m]
- - Crusie flight speed $[\frac{m}{s}]$: automatically calculated from the design machNumber
+ - Crusie flight speed $[\frac{m}{s}]$: automatically calculated from the design mach number
- Contingency [-]: percentage for the reserve of the trip fuel (the fuel necessary for the design range without reserves)
- Cruise flight altitutde [m]: to calculate the air density
--
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