Free engineering calculator

Airflow (CFM) Cooling Calculator

How much air does your heat load need? Enter the power to remove and the air temperature rise you can accept, and get the required volumetric flow - with the altitude derate most quick calculators skip.

T_inQT_in + ΔTV̇ (CFM)altitude h → ρ(h)Q = ρ c_p V̇ ΔT+ margin for bypass / leakage

The diagram is labeled with the same symbols as the input fields below.

The equations this calculator uses

Q = ρ · c_p · V̇ · ΔT  ⇒  V̇ = Q / (ρ c_p ΔT)
ρ(h) = 1.184 · (1 - 2.25577×10⁻⁵ h)⁰·²⁵⁵⁹ kg/m³ (standard atmosphere, 25 °C)
1 m³/s = 2118.88 CFM
Assumptions and limits
  • Sensible heating of dry air at about 25 C inlet: cp = 1006 J/(kg K); density from the standard-atmosphere fit at your altitude.
  • All of the heat load is picked up by the airstream (no radiation or conduction credit).
  • The temperature rise is the BULK air rise from inlet to exhaust, not a component surface rise.
  • Fan selection against system back-pressure is a separate step - this gives required flow only.

Engineering notes

The airflow equation is the workhorse of electronics cooling: at sea level and room temperature it collapses to the familiar rule of thumb CFM ≈ 1.8 × Q / ΔT. This calculator keeps the full form because the shortcuts fail exactly where designs get into trouble - at altitude. Air at 2,000 m is about 18% less dense, so the same CFM carries 18% less heat; at 4,000 m the penalty is a third. Telecom and defense specs call this out; consumer designs discover it in the field.

Choose the allowed rise deliberately. A 10 C rise is a comfortable default for rack equipment; pushing to 20 C halves the required flow but raises every downstream component's inlet temperature and cuts the margin the hottest device sees. And remember the margin input: real chassis leak, recirculate, and bypass air around the heat sinks that need it - 25% is a sensible allowance, tight ducting earns less, open enclosures need more.

What this estimate cannot tell you is the temperature of any specific component - that depends on local velocity, heat-sink design, and the flow path. When the question shifts from "how much air" to "how hot does THIS part get", a conjugate network or CFD-class simulation of the actual layout is the correct escalation.

Frequently asked questions

What is the quick rule of thumb for CFM per watt?

At sea level with a 10 C air rise, roughly 0.18 CFM per watt - i.e. CFM is approximately 1.8 x Q(W) / dT(C). This calculator applies the exact form with density corrected for your altitude.

Does altitude really matter for fan cooling?

Yes: heat capacity per unit VOLUME falls with density. At 2,000 m you need about 22% more CFM for the same load and rise; at 4,000 m about 50% more. High-altitude derating is a standard requirement in telecom and aerospace specifications.

Why is my installed airflow lower than the fan's rating?

Fan ratings are free-delivery (zero back-pressure). Mounted in a real chassis with filters, grilles, and heat sinks, the operating point slides down the P-Q curve - 50-70% of free delivery is typical. Size from the fan curve at your system impedance.