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Leads

Core Members

Reviewers

Progress

Michael Hanley

Isabella Schneider Mackenzie Lui Mohamed Goha

Problem

Problem Statement

Build a lightweight and aerodynamically efficient Aerobody

Goals 

Aerodynamic efficiency will lead to reduced power requirements, this allows us to travel further with the same amount of power while still maintaining a high regard for DFM and DFA

Manufacturability > Performance

Constraints Regulations 

Top surface area of 4m^2 to accommodate array

Max dimensions (L x W x H): 5.0m x 2.2m x 1.6m

Ideal Goals

Coefficient of drag (Cd) < 0.125 (to be somewhat competitive) or =<0.15 (to finish the race)

Frontal area (A) < 1.5 m2 

Requirements

Minimize molds

Minimize cost

Highly durable

Reference Design Materials

Scope

Activity

Must have

  • Research

  • Design

    • Sketches

    • Surface Model

    • Solid Model (Solidworks)

    • Molds

    • Panelization

  • CFD

    • Analysis

    • Verification

  • Detailed design

    • Mounting points

    • Windshield and window cutouts

    • Flanges at connections

    • Wheel Fairings

    • Array Mounting

  • Manufacturing

    • Molds

    • Panels

    • Trimming

    • Finishing

  • Integration

    • Doors

    • Lights

    • Cameras

    • Windshield

    • Windows

  • Mounting to Chassis

  • Sealing all panel gaps

Nice to have

  • Small scale wind tunnel testing

  • (Inset array?)

Not in scope

  • Full scale wind tunnel testing

  • No labels