From 2b72b07c00e1df801adeb43927f0afa56d3fdadf Mon Sep 17 00:00:00 2001 From: Kristina Mazur <kristina.mazur@tum.de> Date: Tue, 28 Jan 2025 10:58:46 +0100 Subject: [PATCH] Update links by removing content --- docs/documentation/sizing.md | 14 +++++++------- 1 file changed, 7 insertions(+), 7 deletions(-) diff --git a/docs/documentation/sizing.md b/docs/documentation/sizing.md index 833c5a9..1214ee8 100644 --- a/docs/documentation/sizing.md +++ b/docs/documentation/sizing.md @@ -48,7 +48,7 @@ The **fuselage_design** module calculates characteristic parameters and generate |Module Version|Language|License|Documentation| |:---:|:---:|:---:|---| -|2.1.0|:simple-cplusplus: |GPLv3|[Link](sizing/fuselage_design/content/index.md)| +|2.1.0|:simple-cplusplus: |GPLv3|[Link](sizing/fuselage_design/index.md)| --- @@ -59,7 +59,7 @@ The **wing_design** module calculates characteristic parameter of the aircraft m |Module Version|Language|License|Documentation| |:---:|:---:|:---:|---| -|2.1.0|:simple-cplusplus: |GPLv3|[Link](sizing/wing_design/content/index.md)| +|2.1.0|:simple-cplusplus: |GPLv3|[Link](sizing/wing_design/index.md)| --- @@ -71,7 +71,7 @@ It takes takes the controllability as wells as the static margin of the aircraft |Module Version|Language|License|Documentation| |:---:|:---:|:---:|---| -|2.1.0|:simple-cplusplus: |GPLv3|[Link](sizing/empennage_design/content/index.md)| +|2.1.0|:simple-cplusplus: |GPLv3|[Link](sizing/empennage_design/index.md)| --- @@ -82,7 +82,7 @@ It takes takes the controllability as wells as the static margin of the aircraft |Module Version|Language|License|Documentation| |:---:|:---:|:---:|---| -|2.1.0|:simple-python: |GPLv3|[Link](sizing/tank_design/content/index.md)| +|2.1.0|:simple-python: |GPLv3|[Link](sizing/tank_design/index.md)| --- @@ -100,7 +100,7 @@ Also the mass properties are analyzed. |Module Version|Language|License|Documentation| |:---:|:---:|:---:|---| -|3.0.0|:simple-cplusplus: |GPLv3|[Link](sizing/propulsion_design/content/index.md)| +|3.0.0|:simple-cplusplus: |GPLv3|[Link](sizing/propulsion_design/index.md)| --- @@ -111,7 +111,7 @@ The **landing_gear_design** module calculates characteristic parameters for the |Module Version|Language|License|Documentation| |:---:|:---:|:---:|---| -|2.1.0|:simple-cplusplus: |GPLv3|[Link](sizing/landing_gear_design/content/index.md)| +|2.1.0|:simple-cplusplus: |GPLv3|[Link](sizing/landing_gear_design/index.md)| --- @@ -123,6 +123,6 @@ It dimensions ATA chapter systems in terms of mass and energy requirement divide |Module Version|Language|License|Documentation| |:---:|:---:|:---:|---| -|2.1.0|:simple-cplusplus: |GPLv3|[Link](sizing/systems_design/content/index.md)| +|2.1.0|:simple-cplusplus: |GPLv3|[Link](sizing/systems_design/index.md)| --- -- GitLab