About this calculator This calculator determines how much an airstream warms when a fan motor operates inside it, following the ASHRAE method for fan motor heat gains. It first computes the motor heat gain from brake horsepower and efficiency, then converts that heat into a temperature rise across the airflow using the altitude-corrected sensible-heat formula. Enter CFM, brake horsepower, motor efficiency, and elevation to size the supply-air temperature offset for draw-through or blow-through fan arrangements where the motor sits in the airstream.
Use when You need the temperature rise added to an airstream by a fan motor mounted within that airstream.
Formula Q = 2545 × (BHP ÷ η)  |  ΔT = Q ÷ (1.08 × DF × CFM)
Variables
CFM Airflow across the fan in cubic feet per minuteBHP Fan brake horsepowerη Motor and drive efficiency, decimal fraction ≤ 1.0Elevation Site elevation in feet — sets the altitude density factorDF Altitude density factor applied to the 1.08 sensible-heat constant
CFM
Airflow across the fan in cubic feet per minute
Brake Horsepower (BHP)
Fan brake horsepower
Motor Efficiency
Decimal fraction of 1.0 or less
Elevation (ft)
Elevation above sea level in feet

Temperature Rise (°F)
Heat Gain (BTU/hr)

How is fan motor heat gain in an airstream calculated?

When a fan motor is located within the airstream it serves, the full electrical input to the motor is added to the air as heat. The heat gain is calculated as Q = 2545 × (BHP / η), where BHP is the fan brake horsepower, η is the motor and drive efficiency as a decimal fraction of 1.0 or less, and 2545 is the conversion factor of BTU/h per horsepower (1 hp = 2,545 BTU/h). That heat gain is then converted to an air temperature rise using the sensible-heat relationship Q = 1.08 × DF × CFM × ΔT, solved for ΔT = Q / (1.08 × DF × CFM). CFM is the airflow in cubic feet per minute and DF is the altitude density factor, DF = (1 − 0.00000687 × Elevation)^5.256, which corrects the standard sea-level constant of 1.08 for reduced air density at higher elevations. Because thinner air carries less heat per unit volume, the same heat gain produces a larger temperature rise at altitude. For example, a fan requiring 10 BHP through a 90% efficient motor at sea level adds Q = 2545 × (10 / 0.9) ≈ 28,278 BTU/hr; across 8,000 CFM that is ΔT = 28,278 / (1.08 × 1.0 × 8,000) ≈ 3.3 °F of supply-air temperature rise.