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This table includes any notable iterations made on the aerobody as well as the results given by CFD sims. (Naming conventions are arbitrary)

All CFD sims are ran with air velocity at 20 m/s.

The frontal area calculations are done using a section view of the car, and are only accurate if the shape curve has 1 local maximum (which it should). The results should then be seen as observations of the decrease in the Cd rather than observations of the Cd as a standalone value, due to the inaccuracy in measuring frontal area. Once the most aerodynamic iteration has been made (relative to the previous iterations), an accurate frontal area calculation will be done, resulting in a more accurate CD.

This being said, our final CFD values will not be representative of real life, so they are only used to analyze the aero performance relative to prior simulations.

Version

Description

(Features)

Pros/Cons

Dimensions (m)

Cd

Frontal Area

V12 (Liam)

Rounded

/Changes

Notes

Dimensions (LWH) (m)

Cd

CdA

Drag Force (N)

MSXV

(for reference)

Wide body (so that other subsystems would 100% fit)

Rounded nose

Curved bottom and top profiles

image-20241028-220949.pngImage Added

4.95 x 1.85 x 1.17 m

Frontal Area

1.35m^2

0.11

0.1485

17.73

V15 (Liam)

Straight top/bottom profiles

Rounded nose

~About 5.75 m^2 for solar array

image-20241028-183500.pngImage Added

View file
nameLiam V15.SLDPRT

Wheelbase length & max steering angle most likely will not comply with ASC 2026 regs (currently 2m and 12 degrees, will need to be around 2.4m and 15 degrees) for a 5.5m car.

  • Need to make aero wider if this is the case, as we do not want dynamic wheel covers opening on small turns.

Need to increase length to accommodate solar

5.5 x 1.35 x 1.13 m

Frontal Area 0.98 m^2

0.13

0.1274

15.30

V16 (Liam)

Straight top/bottom profiles

More aggressive, slightly pointed nose

~5.25 m^2 for solar array

image-20241028-183555.pngImage Added

View file
nameLiam V16.SLDPRT

Not enough room for solar, reduction in Cd and FA is minimal.

Smaller frontal area = larger protruding canopy = more drag

  • To avoid this, canopy needs to be as long as possible (L/h ratio should be around 5-6)

5.5 x 1.29 x 1.13 m

Frontal Area

0.96 m^2

0.125

0.12

14.30

V17 (Liam)

Rounded top/bottom profiles

Less aggressive nose

~5.25 m^2 for solar array

Canopy comes to a point at the back instead of an edge

image-20241028-222207.pngImage Added

View file
nameLiam V17.SLDPRT

Still will need more room for solar, was just experimenting with changing the top/bottom profile shape

5.5 x 1.35 x 1.13 m

Frontal Area

1.02 m^2

0.117

0.119

14.32

V18 (Liam)

Rounded top/bottom profiles

~5.25 m^2 for solar array

Canopy comes to an edge at the back (less flow separation)

image-20241029-021321.pngImage Added

View file
nameLiam V18.SLDPRT

Not achieving significant enough reduction in Cd. Things to try:

  • Making taper near the tail less aggressive (we still want to include the taper to save weight however there is too much flow separation atm.)

  • Larger fillet between roof and canopy

  • Longer canopy

5.5 x 1.35 x 1.17 m

Frontal Area

1.05 m^2

0.116

0.122

14.52

V22 (Liam)

Old canopy style, similar to MSXV

image-20250121-000610.pngImage Added

Old canopy style, similar to MSXV

Roof starts separating from main body right away, allowing more space for solar array (roof not big enough)

5.5 x 1.35 x 1.17 m

Frontal Area

1.01 m^2

0.13

0.13

15.78

V23 (Liam)

Much wider roof compared to V22, allowing more space for solar

very small frontal area, might be too small and not leave enough room for other subsystems

image-20250121-000433.pngImage Added

  • Could only fit 5.6m^2 of 125mm x 125mm solar cells on this roof, will have to make it larger in the next iteration.

  • The junction between the body and the roof may be too aggressive in this model; will attempt to make the transition smoother

5.7 x 1.35 x 1.17 m

Frontal Area

0.945 m^2

0.15

0.142

16.98