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VECTOR / Systems research
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The upper body is already smooth. Remaining drag lies in less visible places — turbulent flow around the rotating wheels, rough underbody surfaces and a wide, separated wake — and each is bound up with cooling, suspension travel and serviceability.
Programme constraint
Overall length and ride height are fixed. Cooling inlet area cannot shrink. Every change must be repeatable on the wind-tunnel model.
Instrumentation
Method
Plan view with flow slices through three zones. Select a zone to see what changes and what the change trades away.
Fictional · illustrativeFIG 1Plan view with flow slices
Wheel zones
Smoother arch lips and an outboard deflector reduce flow shed into the sides.
Cost: Restricts brake ventilation; temperatures must be checked.
FIG 2Relative drag index by zone
BaselineRevised
Index total: 100 → 89. Illustrative, not measured; zones interact so parts do not sum exactly.
| Zone | Baseline index | Revised index | Note |
|---|---|---|---|
| Front and cooling | 22 | 21 | Inlet area fixed |
| Wheel zones | 26 | 22 | Fairing and outboard deflector |
| Underbody | 20 | 17 | Smoothed panels, rear diffuser |
| Wake and tail | 32 | 29 | Slight boat-tail |
| Total | 100 | 89 | Index, not a Cd |
Illustrative relative drag index by zone (baseline total = 100). Invented for the concept; not measured.
Assumptions
Trade-offs
Limitations
What we would verify in real-world testing