oral presentation
TRANSCRIPT
Design, Development and Testing of a Delta wing UAV
Researcher: Reduan SagorSupervisor: Dr Farbod Khoshnoud
Contents1. Personal Motivation
2. Introduction
3. Project Goal
4. Design Specifications?
5. Methodology Applied
6. Results & Discussions
7. Limitations
8. Future Recommendations
2. Introduction
• UAV applications:
Archaeological surveying.
Environmental/meteorology- climate study, storm monitoring etc.
Military- surveillance, air strikes.
Security- crowd monitoring and control.
Law enforcement- traffic monitoring, search and rescue operations.
3. Project Goal
“The aim of this project was to design and manufacture a Delta wing
UAV for surveillance and data acquisition purposes.”
Was the goal achieved?..........................
4. Design Specifications?
• What data can/should be collected?
• Is the wing going to be a flat plate?
• Will the UAV have a fuselage?
• How about a surveillance camera?
• 3D printed UAV sounds good! Hmm..
• Autonomous flight possible?
5. Methodology Applied
• Weight Estimation: Market Research.
• Airfoil Analysis: XFLR5; 2D analysis software; was intended to be used for 3D analysis
of the wing; plots of important parameters in one display interface.
• Wing Analysis: ANSYS Fluent; 3D flow simulation over the wing; manual plotting of
parameters needed.
• CAD Design: CATIA V5 & SOLIDWORKS 2014; SOLIDWORKS used to generate models
for Laser cutting machine.
• Structural Analysis: ANSYS Workbench; FEA analysis of the structure for suitable
material selection.
7. Limitations
• XFLR5 was not used for 3D wing analysis.
• No previous experience of:
3D wing analysis using ANSYS CFD.
Using SOLIDWORKS 2014.
FEA analysis of aircraft structure.
• Limited budget:
Flight Data Recorder (FDR) was not bought.
8. Future Recommendations
• Use of:
Surveillance Camera.
Flight Data Recorder.
Landing Gear.
Traditional take-off and landing using runaway.
• Autonomous flight using ground system.