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Commit 2b72b07c authored by Kristina Mazur's avatar Kristina Mazur
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Update links by removing content

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2 merge requests!55[WEBPAGE] Update style of current unicado page,!17Integrate mkdoxy in CI pipeline
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docs/documentation/sizing.md
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...@@ -48,7 +48,7 @@ The **fuselage_design** module calculates characteristic parameters and generate ...@@ -48,7 +48,7 @@ The **fuselage_design** module calculates characteristic parameters and generate
|Module Version|Language|License|Documentation| |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)|
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...@@ -59,7 +59,7 @@ The **wing_design** module calculates characteristic parameter of the aircraft m ...@@ -59,7 +59,7 @@ The **wing_design** module calculates characteristic parameter of the aircraft m
|Module Version|Language|License|Documentation| |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)|
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...@@ -71,7 +71,7 @@ It takes takes the controllability as wells as the static margin of the aircraft ...@@ -71,7 +71,7 @@ It takes takes the controllability as wells as the static margin of the aircraft
|Module Version|Language|License|Documentation| |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)|
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...@@ -82,7 +82,7 @@ It takes takes the controllability as wells as the static margin of the aircraft ...@@ -82,7 +82,7 @@ It takes takes the controllability as wells as the static margin of the aircraft
|Module Version|Language|License|Documentation| |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)|
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...@@ -100,7 +100,7 @@ Also the mass properties are analyzed. ...@@ -100,7 +100,7 @@ Also the mass properties are analyzed.
|Module Version|Language|License|Documentation| |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)|
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...@@ -111,7 +111,7 @@ The **landing_gear_design** module calculates characteristic parameters for the ...@@ -111,7 +111,7 @@ The **landing_gear_design** module calculates characteristic parameters for the
|Module Version|Language|License|Documentation| |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)|
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...@@ -123,6 +123,6 @@ It dimensions ATA chapter systems in terms of mass and energy requirement divide ...@@ -123,6 +123,6 @@ It dimensions ATA chapter systems in terms of mass and energy requirement divide
|Module Version|Language|License|Documentation| |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)|
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