The Basics of Ventilation, Part Four: Temperature and Altitude adjustments

Altitude and air temperature make a substantial difference in the performance of any ventilation system. The calculations I have provided in the Ventilation Primer, Part Two, are based on sea level and 70 degrees F.

In the calculations, the only variable that needs modifying is VP, Velocity Pressure. The standard calculation is (V/4005) squared.

When applying temperature and altitude corrections, use the following equation: VP = ((V/1096.7) squared) times ‘density of the air in pounds per cubic foot’.

The following table gives standard Density of air in pounds per cubic foot.

Table 2: Temperature and altitude corrections

As an example, let’s go back to example one on the above referenced link and apply both an altitude and temperature correction to the design.


CFM = 1300
Altitude = 5,000 feet above sea level
Temperature = 100 degrees (summer average)
Duct size = 6″ round (or .196 square feet) Use the area of a circle formula (Pi times radius squared) divided by 144.
Total run = 6 feet.
Number of Bends: 0
Loss Factor: 0.11 (from Table 1)

Solve for Velocity: 1300 / .196 = 6632 Feet per Minute
Solve for VP: (6632/1096.7) squared times .059 (from table above) = 2.15
Solve for SP: 2.15 times 6 times .11 = 1.42 inches of pressure

As you can see from the original calculation in example 1 where the calculated static pressure was 1.80 inches, increasing altitude and/or temperature decreases the static pressure in the system. This is due to the fact that at higher altitudes, air is less dense than at sea level.

However, note the temperatures. If your average temperature is below 70 F, your static pressure is going to increase, because cold air is more dense than warm air. This means that your ventilation system is going to be slightly more inefficient in the winter than it will be in the summer.

NOTE: This document is copyright (C) 2009-2015 by Michael Aurelius. Permission is hereby given to readers to use and reproduce this document for their own use only. This document may not be reproduced on any other website or forum without express written permission by the author.


Leave a Reply

Fill in your details below or click an icon to log in: Logo

You are commenting using your account. Log Out / Change )

Twitter picture

You are commenting using your Twitter account. Log Out / Change )

Facebook photo

You are commenting using your Facebook account. Log Out / Change )

Google+ photo

You are commenting using your Google+ account. Log Out / Change )

Connecting to %s