Hot Air Balloon Ascent - 2D Buoyancy Balance and Altitude Profile

Heat the air, find the neutral temperature and watch lift fight weight and drag.

Switch to 3D

Presets

Playback

Parameters

Model checks

The science

Buoyancy of hot air

Archimedes: the envelope of volume V displaces cold air of density ρa, while the hot air inside weighs less. Treating both as ideal gases at the same pressure, the net buoyant force is L = ρa V g (1 - Ta/Ti), with temperatures in kelvin. Lift-off needs L > m g, so the neutral temperature is Ti = Ta / (1 - m/(ρa V)).

Motion, heat and atmosphere

Newton: (m + ρiV + ½ρaV) dv/dt = L - m g - ½ ρa Cd A v|v|, where the extra terms are the carried hot air and the added mass of the sphere, Cd = 0.5 and A = πr². The envelope air obeys ρi V cp dTi/dt = 20 % of the burner power (10 MW at 100 % duty) - loss · (Ti - Ta). Air temperature falls 6.5 K per km and pressure follows the standard-atmosphere law p = p0 (T/T0)5.256, so the same temperature gives less lift higher up.

Honest simplifications: a spherical envelope, constant volume, no wind or turbulence, a fixed burner efficiency and heat-loss coefficient, no vent. Numbers are typical, not those of a particular balloon.

What to try
  • Press Morning lift-off: the balloon stays on the ground until the air passes the neutral temperature, then climbs.
  • Raise the total mass and watch the neutral temperature rise; the heavy preset barely lifts.
  • Use Hold 1000 m: the pilot modulates the burner and the altitude settles.
  • Set the burner to 0 % in flight: heat loss cools the air and the balloon descends.
Altitude against time
Lift and weight against time
Lift against envelope air temperature