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Hot Air Balloon Lifting Force

Reference data and engineering information about hot air balloon lifting force for mechanics applications.

hotairballoonliftingCalculator

Overview

Engineering reference data for Hot Air Balloon Lifting Force in mechanics.

Key Formulas

Newton's Second Law

F=maF = ma

Force = mass × acceleration.

Work

W=FdcosθW = Fd\cos\theta

Work = force × displacement × cos(angle).

Kinetic Energy

Ek=12mv2E_k = \frac{1}{2}mv^2

Energy of motion.

Potential Energy

Ep=mghE_p = mgh

Gravitational potential energy.

Variables

SymbolDescriptionUnit
FFForceN
mmMasskg
aaAccelerationm/s²
vvVelocitym/s

Example Calculation

The lifting force of a hot air balloon can be computed using the primary formula. For a balloon with a volume of V=10m3V = 10 \, \text{m}^3 (353ft3353 \, \text{ft}^3), heated to 100C100^\circ \text{C} (212F212^\circ \text{F}) in surrounding air at 20C20^\circ \text{C} (68F68^\circ \text{F}), the air densities are ρh=0.946kg/m3\rho_h = 0.946 \, \text{kg/m}^3 (0.00184slugs/ft30.00184 \, \text{slugs/ft}^3) and ρc=1.205kg/m3\rho_c = 1.205 \, \text{kg/m}^3 (0.00234slugs/ft30.00234 \, \text{slugs/ft}^3).

The lifting force FlF_l is calculated as:

Fl=V(ρcρh)agF_l = V (\rho_c - \rho_h) a_g

Substituting the values in SI units:

Fl=(10m3)×(1.205kg/m30.946kg/m3)×9.81m/s2=25.4NF_l = (10 \, \text{m}^3) \times (1.205 \, \text{kg/m}^3 - 0.946 \, \text{kg/m}^3) \times 9.81 \, \text{m/s}^2 = 25.4 \, \text{N}

In Imperial units:

Fl=(353ft3)×(0.00234slugs/ft30.00184slugs/ft3)×32.174ft/s2=5.7lbfF_l = (353 \, \text{ft}^3) \times (0.00234 \, \text{slugs/ft}^3 - 0.00184 \, \text{slugs/ft}^3) \times 32.174 \, \text{ft/s}^2 = 5.7 \, \text{lbf}

The mass mm that can be lifted, when the lifting force equals the weight force Fg=magF_g = m a_g, is derived by combining the formulas:

m=Flag=25.4N9.81m/s2=2.6kgm = \frac{F_l}{a_g} = \frac{25.4 \, \text{N}}{9.81 \, \text{m/s}^2} = 2.6 \, \text{kg}

Specific Lifting Force

Specific lifting force refers to the lifting force per unit volume of the balloon, which depends on the temperature difference between the hot air inside and the cold air outside. This parameter is useful for comparing performance under different conditions. For instance, if the balloon air temperature is 60C60^\circ \text{C} and the surrounding air temperature is 20C-20^\circ \text{C}, the specific lifting force is approximately 3.3N/m33.3 \, \text{N/m}^3. Charts are available to visualize this relationship for both SI and Imperial units.

Common Gas Densities

The following table provides the density values for helium and hydrogen, which are often used in lighter-than-air applications alongside hot air.

2 rows
Density of common lifting gases at standard conditions
Gas
Density(kg/m³)
Helium0.1664
Hydrogen0.0899

Source: engineeringtoolbox.com

References