Aero Dynamics

ISA Flight Envelope Engine

Standard Atmosphere (ISA)

Altitude (h)0 m

Velocity (v)250 m/s

Wing Area (S)120 m²

Lift Coeff (C_l)0.50

Drag Coeff (C_d)0.025

Density (ρ)

1.2250

kg/m³

Pressure (P)

101.3k

Temperature (T)

288.1

Kelvin

LIFT (L)

2.30M N

DRAG (D)

114.84k N

Aerodynamic Efficiency

Lift-to-Drag Ratio (L/D)

20.0Efficiency Metric