AERODYNAMICS R&D FACILITY // CHAMBER 04

Virtual Wind Tunnel Chamber

Test surface wake patterns, ground-effect boundary layers, and aerodynamic balance in real-time continuous streamline simulation.

SIMULATION ESTIMATE
STREAMLINES: 220 VECTORSTUNNEL ACTIVE
OPTICAL RIG 60FPS
PRESET:SIDEYAW:0 deg
Air Speed240 km/h66.6 m/s dynamic
Wing Angle18 degHigh-Downforce Flap
Ride Height28 mmVenturi Ground Clearance
DRS FlapCLOSEDDrag Reduction Slot
Dynamic Readouts
LIVE SYNC
Total Downforce
2460N
SIMULATED
Aerodynamic Drag
890N
SIMULATED
Efficiency (L/D)
2.76RATIO
Telemetry Parameters
240 km/h
100 km/h230 km/h (MED)360 km/h
18 deg
8 deg (Low Drag)32 deg (High Downforce)
28 mm
18 mm (Venturi Peak)45 mm (High Rake)
DRS Wing Slot Open-35% Drag penalty / -22% Downforce
Telemetry Matrix / SIM-LABSPEC-F1-CFD

Aero Package Aero Comparisons

Direct computational comparison between high-downforce Monaco configurations and low-drag Monza speedway packages. All aerodynamic, ride height, and underfloor ground-effect metrics are calibrated for chassis simulation.

RIG_01
Downforce Generation
@ 250 km/h
Monaco Spec1,840 kg
Monza Spec1,120 kg

+64.3% vertical loading for street circuit adhesion

RIG_02
Aerodynamic Drag Load
@ 250 km/h
Monaco Spec584 kg
Monza Spec256 kg

-56.1% parasitic air resistance along high-speed straights

RIG_03
Efficiency Quotient (L/D)
Lift-to-Drag Index
Monaco Spec3.15
Monza Spec4.38

Monza achieves peak thermodynamic efficiency profile

Parametric Flow & Chassis Differential

Comparative values measured at dynamic ride height stabilization

SIMULATED DATA
Chassis ParameterSubsystemMonaco (High Downforce)Monza (Low Drag)Differential
Front Wing Flap Angle
Turn-in authority vs straightline drag
Front Aero38.5 deg14.2 deg+24.3 deg
Rear Wing Mainplane Camber
Downforce ceiling vs DRS delta speed
Rear AeroHigh Camber (28 deg)Skinny Spoon (6 deg)+22.0 deg
Front Ride Height (Static)
Kerb strike tolerance vs throat sealing
Suspension24.0 mm18.5 mm+5.5 mm
Rear Ride Height (Static)
Underbody expansion angle control
Suspension62.0 mm44.0 mm+18.0 mm
Venturi Throat Negative Pressure
Floor suction through slow hairpins
Underfloor-14.8 kPa-9.2 kPa-5.6 kPa
Diffuser Expansion Area Ratio
Diffuser pumping at low dynamic head
Underfloor3.42 : 12.85 : 1+0.57 : 1
Total Downforce @ 250 km/h
Corner apex minimum speed capability
Global Output1,840 kg1,120 kg+720 kg
Drag Coefficient (CdA)
Terminal speed on Rettifilo straight
Global Output1.42 m20.78 m2+0.64 m2
Aero Efficiency (L/D Ratio)
Energy trade-off efficiency factor
Global Output3.154.38-1.23
Simulated Top Speed (DRS Active)
Speed trap ranking & overtaking viability
Telemetry Output292 km/h354 km/h-62 km/h
Monaco: Maximum Downforce, Steep Angle of AttackMonza: Low Camber, Minimized Induced Drag
CFD baseline: 250 km/h, 15 deg C ambient, sea level air density

Aerodynamic Configuration Directive

Switching to the Monaco specification trades 62 km/h in top speed for a +720 kg gain in high-speed lateral cornering stability. The venturi throat suction remains optimized for curbs and low-speed hairpin rotation.