Boost & Pressure Ratio Calculator

Turn a boost gauge reading into pressure ratio, absolute manifold pressure, bar and kPa, corrected for altitude, the numbers you need to read a turbo compressor map.

Pressure ratio
1.82
what you read on a compressor map
Absolute manifold pressure
26.7 psia
184 kPa · 1.84 bar abs
Boost in other units
0.83 bar
83 kPa gauge
Ambient pressure here
14.70 psia
0% less air than sea level

Gauge vs absolute pressure

A boost gauge reads pressure above the air around you. The engine (and a compressor map) cares about absolute pressure: boost plus atmospheric pressure. At sea level, 12 psi of boost is about 26.7 psia; at 5,280 ft the same 12 psi is only about 24.1 psia, because there's less air to start with.

Pressure ratio

pressure ratio = (boost + ambient) ÷ ambient. It's the vertical axis of a compressor map. The same boost at altitude means a higher pressure ratio, so the turbo works harder and runs hotter. That's why a turbo that's fine at sea level can run out of breath in the mountains.

Altitude and NA engines

A naturally aspirated engine makes power roughly in proportion to absolute pressure, so it loses about 3% per 1,000 ft. A turbo car with boost control can make most of that back, so altitude hurts it far less.