T-6BTrainer
≡≡≡≡ AERODYNAMICS · WIND TUNNEL TERMINAL · v2.0 ≡≡≡≡
FOUR FORCES
// REAL-TIME TELEMETRY
LIFT 0 N
WEIGHT 12000 N
THRUST 0 N
DRAG 0 N
→ LEVEL FLIGHT

LIFT EQUATION

L = ½ · ρ · V² · S · CL
ρ air density 1.225 kg/m³
V airspeed 50 m/s
2500
S wing area 16
CL lift coef 0.78
L = 0 N

FLIGHT PARAMETERS

ANGLE OF ATTACK (α)5°
AIRSPEED (V)50 m/s
AIR DENSITY (ρ)1.225
WING AREA (S)16
► DRAG TO ROTATE · SCROLL TO ZOOM
► CHORD LINE = YELLOW · FREE STREAM = CYAN

FIELD NOTES

BERNOULLI + NEWTON. Faster flow over the curved top creates lower pressure (Bernoulli). The wing also deflects air downward — equal and opposite reaction (Newton's 3rd law). Both descriptions are correct, just different lenses on the same physics.
> INIT WIND_TUNNEL.SYS ............................ OK
> LOADING NACA 2412 PROFILE ....................... OK
> ALLOC PARTICLE_FIELD [4096] ..................... OK
> BIND VORTEX_SOLVER (KUTTA-JOUKOWSKI) ............ OK
> CALIBRATE FORCE VECTORS ......................... OK
> ENGAGE PHOSPHOR DISPLAY ......................... OK
>
> READY.