Create a presentation for the diploma thesis

Presentation structure:

1. Title slide
Title of the diploma project, full name of the student, group AT-21, supervisor, Igor Sikorsky Kyiv Polytechnic Institute, Department of TVLA.

2. Relevance of the work
Explain why a rear wing is needed for the front-wheel-drive Mercedes-Benz A200 W176: increased stability, enhanced rear axle grip, use in Time Attack.

3. Goals and objectives of the project
Goal: to develop the design, technology, and equipment for manufacturing a wing that generates about 1.8 kN of downforce at a speed of 60 m/s and attaches to the body without welding or cutting body elements.
Show the main tasks: analysis of analogs, material selection, design development, modeling, manufacturing technology, equipment.

4. Analysis of analogs and concept selection
Show examples: Volkswagen Golf GTI TCR, swan-neck mounts, end plates, angle of attack adjustment. Explain that the adopted scheme is a separate profile with a top swan-neck mount.

5. Profile and geometry selection of the wing
Explain the choice of profile S1223, width 1700 mm, chord 400 mm, presence of end plates, and angle of installation adjustment.

6. Overall design of the wing
Show a 3D model in assembly. Highlight the main profile, end plates, swan-neck supports, main supports, lower beam, upper crossbar, struts, and bolt connections.

7. Load transfer scheme to the body
Explain the load transfer path: profile → brackets → swan-neck → main supports → crossbars → structural elements of the body. Emphasize that the attachment is bolted, without welding to the body.

8. Topological optimization of supports
Show the initial and optimized geometry of the main support and swan-neck. Explain that optimization allowed for weight reduction while retaining material in load-bearing areas.

9. Aerodynamic modeling
Show Flow Simulation: calculation area, flow direction, speed 60 m/s, four adjustment positions. The main result — position 75.5° provides about 1779.9 N, or approximately 181 kgf of downforce.

10. Strength check of attachment elements
Show stress results and safety margins for the swan-neck and main support. Indicate that the minimum safety margin for the swan-neck is 1.6, and for the main support — 15. Conclude that the most critical part is the swan-neck.

11. Manufacturing technology and equipment
Show the technology: foam core, CFRP skins, Mylar film, vacuum sealing, vacuum infusion of end plates, CNC machining of aluminum parts, TIG welding of the lower beam, assembly stand.

12. General conclusions
Summarize briefly: the wing design has been developed, materials justified, the required downforce of about 180 kgf achieved, structural elements checked, manufacturing technology and equipment proposed.

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I will send the actual work in personal correspondence.