Turbo Airflow & Compressor Sizing
The two numbers a compressor map needs: the mass flow your power target burns, and the pressure ratio the engine needs to swallow it at that speed.
Air flow in pounds a minute and corrected to the map’s reference conditions, the pressure ratio after filter and intercooler losses, the manifold pressure and boost, and the charge density ratio.
Example: 400 hp at 0.55 BSFC and 12 : 1 needs 44 lb/min; through a 2.0 L at 6 500 rpm that is 28.7 psi of boost, a pressure ratio of 3.16, and 42.9 lb/min corrected.
A compressor map
has two axes.
How power becomes mass flow, how mass flow becomes a pressure ratio, and why the flow has to be corrected before you plot it.
From power to air
An engine burns fuel in proportion to the power it makes — that proportion is the brake specific fuel consumption — and it needs air in proportion to the fuel, at the air-fuel ratio it runs. Two multiplications therefore turn a power target into a mass flow of air: power × BSFC × AFR. Mass flow, not cubic feet a minute, is what a compressor map is drawn in, and the two numbers you multiply by are the two that differ most between engines, so neither is assumed here. A boosted petrol engine at full load is thirstier and richer than the same engine atmospheric, and using its naturally aspirated figures understates the turbo you need.
From air to pressure ratio
The engine swallows a fixed volume a cycle — displacement × speed ÷ two for a four-stroke, times its volumetric efficiency — so carrying the required mass flow through it sets the density, and the ideal gas law turns density into a manifold pressure. The compressor has to make that pressure plus whatever the intercooler and piping lose, starting from atmospheric minus whatever the filter costs; both losses are charged twice, once as pressure to make and once as pressure the engine never sees. Finally the flow is corrected to the map’s reference conditions, because a map is plotted in corrected pounds a minute and reading raw flow against it sizes the wrong turbo.
Limits
Steady state at one engine speed, and the compressor side only. No turbine, no A/R ratio, no wastegate, no spool behaviour, no exhaust back pressure and no efficiency island — this page gives you the point to plot, not the turbo to buy, and the outlet temperature that pressure ratio implies belongs to the boost and pressure ratio page. Air is treated as an ideal gas at R = 287.05 J/(kg·K). BSFC, air-fuel ratio and volumetric efficiency are your inputs from your own engine, and a VE measured on an atmospheric dyno is optimistic here. Nothing leaves the browser; the same four anonymous usage counts as the rest of the site apply.
SOURCES
- Air flow = power × BSFC × air-fuel ratio; MAP = ṁ·R·T ÷ (V_d·N/2·VE); corrected flow × √(T/T_ref) ÷ (P/P_ref); BSFC, AFR and VE are your inputs, no turbine side is modelled
Last reviewed 22 September 2026. How results are checked: How we verify.