Hypercar Aero Digital Twin

SYS.VER // 7.0.0-LMH // AEROSPACE GRADE SIMULATION
Inlet Velocity ($v_{\infty}$) 280 km/h
DRS Flap Deflection: 0.0°
Dynamic Pressure ($q$): 3.71 kPa
Downforce ($F_z$): 3210 N
Aero Drag ($F_x$): 840 N
Efficiency ($L/D$): 3.82
Aero Balance (F/R): 44.2 %
Drag Power Loss: 65.3 kW

LMH Architecture // Technical Matrix

Algorithmic Monocoque Generation The central chassis utilizes procedural non-linear G2 curvature continuity matching FIA WEC Le Mans Hypercar regulations. Surface continuity is audited via dynamic reflection zebra mapping and real-time scalar pressure coefficient ($C_p$) shading.
Multi-Element Active Aerodynamics (DRS) The rear wing assembly incorporates a dual-element high-downforce airfoil with a dynamic low-drag actuator. Hydraulic kinematic motion reduces total profile drag ($F_x$) by ~35% while suppressing trailing vortex shedding.
Particle Streamline CFD Solver Simulates dynamic compressible flow using particle velocity integration bounded by the chassis geometry. Streamline color mapping reflects localized vector kinetic energy gradients.