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Wind Tunnel Test Campaign

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Photograph of the SUBLIME model installed in the ARA Transonic Wind Tunnel

Powered, BLI360 configuration in the ARA Transonic Wind Tunnel (TWT)

The following data was collected:

  • AIP distortion maps
  • Fuselage surface pressures including boundary layer development
  • Rear fuselage loads with force balance
  • Wake rake total pressure maps
  • Oil flow surface visualisation
  • Particle Image Velocimetry (PIV) off-body flow visualisation

Project Outcomes

  • CFD Study of Fan Performance with Distortion
    • Blade Design
    • Preliminary Design Procedure
    • Selected Design
  • Evaluating BLI Performance
    • Boundary Layer Ingestion Fundamentals
    • Performance Evaluation
    • Performance Evaluation Approach
    • Work-Energy Relationships of Flight
  • Optimal Design of BLI Architecture
    • 2D Axisym Design Space Investigation
    • 3D Refinement Optimization
    • Engine Deck Modelling
    • Performance Metrics
  • Wind Tunnel Model Design
    • Interesting Parts
    • Manufacturing Review
    • Model Concept
    • Model Specification
  • Wind Tunnel Test Campaign
    • Boundary Layer Development
    • Flow Visualisation
    • Reference Wake Processing

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