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Half module - Webbed Dashboard
▼ Half module - Webbed
☰ \( H_{\text{half, webbed}} \) Half module - Webbed rim height (m) 0.1
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Purpose: Matches the standard Z-axis height.
Logic: Ensures seamless integration within the staggered layer sequence.
Type: Calculated (Math Output)
Render on Grids: None
Mathematical Formula:
$$H_{\text{half, webbed}} = H_{\text{solid, flat}}$$
Python Logic: v["Solid Module - Flat height (m)"]
Live Evaluation: [ROUTE: STATIC/GLOBAL] 0.1000 = 0.1000
☰ \( L_{\text{half, webbed}} \) Half module - Webbed rim length (m) 1
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Purpose: Matches the standard longitudinal pitch.
Logic: Ensures all connector points align with the primary structural spines.
Type: Calculated (Math Output)
Render on Grids: None
Mathematical Formula:
$$L_{\text{half, webbed}} = L_{\text{solid, flat}}$$
Python Logic: v["Solid Module - Flat length (m)"]
Live Evaluation: [ROUTE: STATIC/GLOBAL] 1.0000 = 1.0000
☰ \( W_{\text{half, webbed}} \) Half module - Webbed rim width (m) 0.5
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Purpose: Defines the half-width lateral dimension.
Logic: Required for secondary bracing and joint-offsetting (brick-bonding).
Type: Calculated (Math Output)
Render on Grids: None
Mathematical Formula:
$$W_{\text{half, webbed}} = W_{\text{half}}$$
Python Logic: v["Half Module width (m)"]
Live Evaluation: [ROUTE: STATIC/GLOBAL] 0.5000 = 0.5000
☰ \( H_{\text{half, webbed}} \) Half module - Webbed inside height (%)
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Purpose: Sets the membrane thickness for the half-module.
Logic: Sets the stiffness-to-weight ratio for the central web, essential for stability.
Type: Manual Entry
Render on Grids: None
Mathematical Formula:
Adjustable user input
Python Logic: N/A
Live Evaluation: N/A (Input Variable)
☰ \( H_{\text{half, webbed}} \) Half module - Webbed inside height (m) 0.04
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Purpose: The physical thickness of the half-module's web.
Logic: The as-machined thickness of the internal carbon fiber diaphragm.
Type: Calculated (Math Output)
Render on Grids: None
Mathematical Formula:
$$H_{\text{half, webbed}} = H_{\text{solid, flat}} \times H_{\text{half, webbed}}$$
Python Logic: v["Solid Module - Flat height (m)"] * v["Half module - Webbed inside height (%)"]
Live Evaluation: [ROUTE: STATIC/GLOBAL] 0.1000 * 0.4000 = 0.0400
☰ \( L_{\text{half, webbed}} \) Half module - Webbed inside length (m) 0.8
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Purpose: The length of the half-module's mass-reduction void.
Logic: Establishes the Y-axis boundary for the hollowed-out center.
Type: Calculated (Math Output)
Render on Grids: None
Mathematical Formula:
$$L_{\text{half, webbed}} = L_{\text{half, webbed}} - ( W_{\text{border}} \times 2 )$$
Python Logic: v["Half module - Webbed rim length (m)"] - ( v["Module Border Width (m)"] * 2 )
Live Evaluation: [ROUTE: STATIC/GLOBAL] 1.0000 - ( 0.1000 * 2 ) = 0.8000
☰ \( W_{\text{half, webbed}} \) Half module - Webbed inside width (m) 0.3
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Purpose: The width of the half-module's mass-reduction void.
Logic: Establishes the X-axis boundary for the hollowed-out center.
Type: Calculated (Math Output)
Render on Grids: None
Mathematical Formula:
$$W_{\text{half, webbed}} = W_{\text{half, webbed}}-(W_{\text{border}} \times 2)$$
Python Logic: v["Half module - Webbed rim width (m)"]-(v["Module Border Width (m)"]*2)
Live Evaluation: [ROUTE: STATIC/GLOBAL] 0.5000-(0.1000*2) = 0.3000
☰ \( V_{\text{half, webbed}} \) Half module - Webbed inside volume (m3) 0.0096
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Purpose: The 3D volume of the half-module's thin central web.
Logic: Calculates the material volume of the thinned central section.
Type: Calculated (Math Output)
Render on Grids: None
Mathematical Formula:
$$V_{\text{half, webbed}} = H_{\text{half, webbed}} \times L_{\text{half, webbed}} \times W_{\text{half, webbed}}$$
Python Logic: v["Half module - Webbed inside height (m)"] * v["Half module - Webbed inside length (m)"] * v["Half module - Webbed inside width (m)"]
Live Evaluation: [ROUTE: STATIC/GLOBAL] 0.0400 * 0.8000 * 0.3000 = 0.0096
☰ \( M_{\text{half, webbed}} \) Half module - Webbed inside weight (kg) 17.28
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Purpose: The weight of the half-module's central web.
Logic: The weight contribution of the central stabilizing membrane within the half-unit.
Type: Calculated (Math Output)
Render on Grids: None
Mathematical Formula:
$$M_{\text{half, webbed}} = V_{\text{half, webbed}} \times \text{Fossil Carbon Fibre Density (kg.m3)}$$
Python Logic: v["Half module - Webbed inside volume (m3)"] * v["Fossil Carbon Fibre Density (kg.m3)"]
Live Evaluation: [ROUTE: STATIC/GLOBAL] 0.0096 * 1,800.0000 = 17.2800
☰ \( V_{\text{half, webbed}} \) Half module - Webbed rim volume (m3) 0.026
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Purpose: The 3D volume of the solid half-frame.
Logic: Calculates the displacement of the solid perimeter that resolves the localized shear loads.
Type: Calculated (Math Output)
Render on Grids: None
Mathematical Formula:
$$V_{\text{half, webbed}} = ( H_{\text{half, webbed}} \times L_{\text{half, webbed}} \times W_{\text{half, webbed}} ) - ( H_{\text{half, webbed}} \times L_{\text{half, webbed}} \times W_{\text{half, webbed}} )$$
Python Logic: ( v["Half module - Webbed rim height (m)"] * v["Half module - Webbed rim length (m)"] * v["Half module - Webbed rim width (m)"] ) - ( v["Half module - Webbed rim height (m)"] * v["Half module - Webbed inside length (m)"] * v["Half module - Webbed inside width (m)"] )
Live Evaluation: [ROUTE: STATIC/GLOBAL] ( 0.1000 * 1.0000 * 0.5000 ) - ( 0.1000 * 0.8000 * 0.3000 ) = 0.0260
☰ \( M_{\text{half, webbed}} \) Half module - Webbed rim weight (kg) 46.8
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Purpose: The weight of the half-unit's reinforced shell.
Logic: Quantifies the static mass of the outer perimeter for the half-block.
Type: Calculated (Math Output)
Render on Grids: None
Mathematical Formula:
$$M_{\text{half, webbed}} = V_{\text{half, webbed}} \times \text{Fossil Carbon Fibre Density (kg.m3)}$$
Python Logic: v["Half module - Webbed rim volume (m3)"] * v["Fossil Carbon Fibre Density (kg.m3)"]
Live Evaluation: [ROUTE: STATIC/GLOBAL] 0.0260 * 1,800.0000 = 46.8000
☰ \( \Sigma M_{\text{half, webbed}} \) Half module - Webbed total weight (kg) 64.08
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Purpose: The final, optimized weight for the half-module.
Logic: Critical for ensuring the Gross System Mass totals remain highly accurate when closing the structural seams.
Type: Calculated (Math Output)
Render on Grids: None
Mathematical Formula:
$$\Sigma M_{\text{half, webbed}} = M_{\text{half, webbed}} + M_{\text{half, webbed}}$$
Python Logic: v["Half module - Webbed rim weight (kg)"] + v["Half module - Webbed inside weight (kg)"]
Live Evaluation: [ROUTE: STATIC/GLOBAL] 46.8000 + 17.2800 = 64.0800