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Domain Configuration

The computational domain defines the 3D space where your CFD simulation will be performed. The Navier AI Platform provides intelligent domain sizing that automatically adapts to your geometry.

Domain Sizing Philosophy

Why Domain Size Matters

  • Boundary Effects: Domain boundaries can artificially influence your results
  • Accuracy: Insufficient domain size leads to incorrect pressure and velocity fields
  • Efficiency: Oversized domains waste computational resources
  • Convergence: Proper sizing ensures stable, converged solutions

Platform Approach

The platform automatically calculates optimal domain dimensions based on:
  • Geometry bounding box analysis
  • Flow physics requirements
  • Industry best practices
  • Computational efficiency

Preset Configurations

Small Domain

Use Cases: Initial testing, simple geometries, quick results
Multipliers (based on characteristic length):
- Upstream: 8× 
- Downstream: 15×
- Lateral: 6×
- Vertical: 4×

Typical Applications:
- Basic validation studies
- Preliminary design analysis
- Simple external flow

Medium Domain

Use Cases: Standard simulations, most engineering applications
Multipliers (based on characteristic length):
- Upstream: 10×
- Downstream: 20×
- Lateral: 8×
- Vertical: 6×

Typical Applications:
- Production vehicle analysis
- Drone performance studies
- Building aerodynamics
- General external flow

Large Domain

Use Cases: Wake studies, high-accuracy requirements, research
Multipliers (based on characteristic length):
- Upstream: 15×
- Downstream: 30×
- Lateral: 12×
- Vertical: 8×

Typical Applications:
- Detailed wake analysis
- Academic research
- Validation against experiments
- High-precision simulations

Custom Domain Configuration

Manual Sizing

For specialized applications, specify custom multipliers:
Guideline: 5-15× characteristic length
  • : Minimum for attached flow
  • 10×: Standard for most applications
  • 15×: High accuracy or complex inlet conditions
Considerations:
  • Allows flow development before reaching geometry
  • Prevents inlet boundary condition artifacts
  • Required for realistic approach flow
Guideline: 10-30× characteristic length
  • 10×: Minimum for basic pressure recovery
  • 20×: Standard for complete wake capture
  • 30×: Detailed wake analysis and far-field effects
Considerations:
  • Captures pressure recovery region
  • Prevents outlet boundary effects
  • Essential for accurate drag calculation
Guideline: 5-15× characteristic width
  • : Minimum for symmetric flows
  • : Standard for external aerodynamics
  • 15×: Crosswind studies or asymmetric effects
Considerations:
  • Prevents side boundary interference
  • Allows for flow expansion around geometry
  • Critical for lift-generating bodies
Guideline: 3-10× characteristic height
  • : Ground effect studies (wind tunnel)
  • : Standard atmospheric boundary layer
  • 10×: High-altitude or unconstrained flow
Considerations:
  • Ground plane simulation requirements
  • Atmospheric boundary layer development
  • Vertical flow structures (updrafts, downdrafts)

Flow Direction Setup

Coordinate System

  • X-axis: Primary flow direction (streamwise)
  • Y-axis: Lateral/crosswind direction (spanwise)
  • Z-axis: Vertical direction (normal to ground)

Direction Selection

X-Direction Flow

Most Common
  • Standard for vehicles, aircraft
  • Streamwise flow analysis
  • Typical wind tunnel setup

Y-Direction Flow

Crosswind Analysis
  • Vehicle stability studies
  • Building wind loading
  • Lateral flow effects

Z-Direction Flow

Vertical Flow
  • Helicopter rotor analysis
  • Vertical take-off aircraft
  • Stack emissions

Characteristic Length Calculation

Automatic Calculation

The platform automatically determines characteristic length from:
  • Vehicles: Overall length
  • Aircraft: Wingspan or chord length
  • Buildings: Maximum dimension
  • General: Largest bounding box dimension

Manual Override

You can specify custom characteristic length for:
  • Non-standard reference dimensions
  • Industry-specific conventions
  • Validation against specific test cases

Common Reference Lengths

Application Examples:
- Automotive: Vehicle length (4-5m)
- Aircraft: Wing chord (1-10m)  
- Drones: Rotor diameter (0.2-2m)
- Buildings: Height or width (10-100m)

Domain Positioning

Automatic Centering

  • Geometry automatically centered in lateral (Y) and vertical (Z) directions
  • Upstream/downstream positioning based on flow direction
  • Ground plane handling for surface vehicles

Manual Positioning

Available adjustments:
  • Translation: Move geometry within domain
  • Ground Clearance: Adjust height above ground plane
  • Flow Alignment: Rotate geometry relative to flow direction

Boundary Identification

Automatic Patch Creation

The platform creates six domain boundary patches:
  • Inlet: Upstream boundary (flow enters)
  • Outlet: Downstream boundary (flow exits)
  • Sides: Left and right lateral boundaries
  • Top: Upper vertical boundary
  • Bottom: Lower boundary (often ground plane)

Naming Convention

Boundary Patch Names:
- inlet (upstream face)
- outlet (downstream face)
- side_left (negative Y face)
- side_right (positive Y face)
- top (positive Z face)  
- bottom (negative Z face, ground)

Validation and Quality Checks

Automatic Validation

The platform checks for:
  • Minimum Distances: Ensures adequate spacing
  • Aspect Ratios: Prevents extreme domain shapes
  • Boundary Clearance: Verifies geometry doesn’t touch boundaries
  • Physical Realism: Checks for reasonable dimensions

Warning Indicators

Common Warnings:
  • Domain too small: Boundary effects likely
  • Extreme aspect ratio: Poor mesh quality possible
  • Geometry near boundary: Artificial flow constraint
  • Unrealistic dimensions: Check geometry scale

Advanced Domain Features

Ground Plane Modeling

  • Automatic Detection: Platform identifies ground-based vehicles
  • Clearance Setting: Specify ride height or ground gap
  • Boundary Conditions: Appropriate wall/symmetry conditions

Multi-Body Domains

  • Component Spacing: Automatic domain sizing for assemblies
  • Interference Effects: Domain sized to capture interactions
  • Individual Analysis: Option to analyze components separately

Wind Tunnel Simulation

  • Tunnel Walls: Constrained domain boundaries
  • Blockage Effects: Account for tunnel cross-section
  • Test Section: Realistic wind tunnel geometry

Best Practices

Domain Size Guidelines

Conservative Approach

When to use larger domains:
  • High-accuracy requirements
  • Research applications
  • Validation studies
  • Unknown flow characteristics

Efficient Approach

When smaller domains are acceptable:
  • Preliminary analysis
  • Parametric studies
  • Known flow patterns
  • Resource constraints

Performance Optimization

  • Start Small: Begin with medium domain, increase if needed
  • Mesh Density: Balance domain size with mesh resolution
  • Convergence: Monitor for boundary effects in results
  • Validation: Compare different domain sizes for key metrics

Common Domain Setups

Automotive Analysis

Typical Setup:
- Upstream: 3-5× vehicle length
- Downstream: 10-15× vehicle length
- Width: 3-5× vehicle width
- Height: 3-4× vehicle height
- Ground clearance: 0.05-0.1m

Aircraft Analysis

Typical Setup:
- Upstream: 5-10× chord length
- Downstream: 15-25× chord length
- Span: 5-8× wingspan
- Height: 5-10× chord length
- Symmetry plane option available

Building Analysis

Typical Setup:
- Upstream: 5-10× building height
- Downstream: 15-20× building height
- Width: 5-8× building width
- Height: 6-10× building height
- Atmospheric boundary layer

Next Step: With your domain configured, proceed to Mesh Configuration to set up your computational mesh with intelligent refinement zones.