Airflow / CRAC
Enter the heat load (kW) and the air ΔT (supply→return) and I compute the required airflow (CFM and m³/s) and the tons of refrigeration to size your CRAC/CRAH.
Calculation breakdown
| Quantity | Value | Formula |
|---|
How it is calculated · airflow, m³/s and tons
1. Dry air at sea level: density
ρ = 1.2 kg/m³, specific heat cp = 1005 J/(kg·K).
2. SI airflow:
Q(m³/s) = P(W) ÷ (ρ · cp · ΔT), with ΔT in K (= °C).
3. To CFM: CFM = Q(m³/s) × 2118.88.
Equivalent imperial formula: CFM = kW × 3412 ÷ (1.08 × ΔT_°F),
with ΔT_°F = ΔT_°C × 1.8 (they agree within ±0.1 %).
4. Cooling:
tons = kW ÷ 3.517 (1 TR = 3.517 kW) ·
BTU/h = kW × 3412.14.
5. This airflow is the theoretical minimum for the given ΔT: it excludes recirculation, leakage through poorly sealed containment and CRAC headroom. Size the unit with margin and validate the real ΔT with probes on supply and return.
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How it works
The calculator converts the heat load of a room or rack (in kW) into the airflow required to remove it, based on the ΔT between supply and return air. It reports the flow in CFM and m³/s, plus the load expressed in tons of refrigeration and BTU/h, which is how CRAC/CRAH units are specified.
The model is the thermal balance of air: Q(m³/s) = P(W) ÷ (ρ · cp · ΔT), with dry-air density ρ = 1.2 kg/m³ and specific heat cp = 1005 J/(kg·K) at sea level. The CFM conversion uses 1 m³/s = 2118.88 CFM (equivalent to the imperial formula CFM = kW × 3412 ÷ (1.08 × ΔT_°F)), and cooling is expressed with 1 ton = 3.517 kW. The result is the theoretical minimum: it does not include recirculation, containment leakage or unit margin.
Example: how much air does a 10 kW row need at a 12 °C ΔT?
- SI flow:
10,000 W ÷ (1.2 × 1005 × 12) = 0.691 m³/s. - In CFM:
0.691 × 2118.88 ≈ 1,464 CFM. - Cooling:
10 ÷ 3.517 = 2.84 tons(about 34,121 BTU/h). - The CRAC must move at least 1,464 CFM at that ΔT; in practice you size with headroom.