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Transcript of Thesis
Improving wing design
MUAV design Problem Definition Pixel Resolution: 50 micron (m)
Source Voltage: 60kV Surfacing
Assembly & Scaling Creating the Model Laminar
Unstructured Mesh CFD X-ray a viable method for geometry
CFD results show effects of corrugations Conclusion Leading edge vortices / Vortex shedding
Excellent aerodynamic performance
Wings like sails Background MicroXCT-400 Reconstructed via XCT-400
Filtered via Vg-Studio Max Cross Sections
Spline Extrapolation Fore and Aft wings Creating the Model Vortex Recirculation in corrugations
LEV / TEV circulation Results Natalie Klomp Micro-CT based CFD Analysis of Insect Flight z3309010 Supervisors: Dr N. Tsafnat & Dr G. Doig Questions? Filtering
Paint Tool Amira Cleanup Vortex distribution over wing
CLmax at High AOA Results Future Work Transient Analysis
Flapping Wing Analysis Thank you to my supervisors:
Dr Naomi Tsafnat and Dr Graham Doig LEV / TEV circulating over wing