Speed Flying Micro-Climate & Terrain Proximity Physics Simulator

AIRSPEED 102.5 km/h

SINK RATE -4.8 m/s

CLEARANCE 4.20 m

REACTION WINDOW 148 ms

STEERING BANK ANGLE (A/D) 0°

GLIDE TRIM (W/S) NORMAL (L/D 3.8)

WING AREA (WING LOADING) 8.0 m²

🌪️ Micro-Climate Canyon Presets & Vectors

Alpine Ridge Sprint Steep mountain slope, steady 12.5 m/s ridge wind, high slope lift.

Venturi Canyon Squeeze Narrow gorge producing 1.8x wind amplification and high shear.

Shear Layer Microburst Sudden sink drop & thermal turbulence mid-trajectory.

RIDGE WIND SPEED 12.5 m/s

CANYON VENTURI COMPRESSION 1.45x

THERMAL UPDRAFT STRENGTH 3.2 m/s

📈 Real-time Flight Telemetry

GROUND CLEARANCE

4.2 m

Limit: > 2.0 m

G-FORCE LOAD

1.28 G

Turn roll pressure

EFFECTIVE L/D RATIO

3.82

Glide efficiency

WIND SPEED OVER WING

118 km/h

Venturi amplified

ALTITUDE (MSL)

1,742 m

Launch: 1,800 m

PILOT REACTION MARGIN

148 ms

Distance / Airspeed

FLIGHTPATH TRACK SCRUBBER T+ 8.4s

0.0s (Launch) LIVE SIMULATION End of Canyon

🧠 Boundary Layer Micro-Climate Aerodynamics

Speed flying combines high wing-loading (10+ kg/m²) with low glide ratios (L/D ~ 3 - 5) to maintain controllable high speeds close to terrain.

Venturi Effect in Gorges: Narrow canyon geometry forces wind velocity vectors to multiply according to mass continuity: V₂ = V₁ · (A₁ / A₂).

Reaction Window: At 100 km/h (27.8 m/s), a 4-meter ground clearance provides a reaction margin of under 150 ms before collision on trajectory divergence.