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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