Can someone offer a really good explanation of the difference between pressure altitude and density altitude?

As an example for discussion (using a place not at sea level), suppose I was at Telluride, Colorado (TEX) which has an altimeter setting today of 29.87 and an airport elevation of 9078 ft. I think the pressure altitude is:

29.92-29.87=0.05

0.05*1000= 50 ft

50 ft + 9078 ft = 9128 ft

If this is correct, where does density alt. come into play?

As an example for discussion (using a place not at sea level), suppose I was at Telluride, Colorado (TEX) which has an altimeter setting today of 29.87 and an airport elevation of 9078 ft. I think the pressure altitude is:

29.92-29.87=0.05

0.05*1000= 50 ft

50 ft + 9078 ft = 9128 ft

If this is correct, where does density alt. come into play?

"We have clearance Clarence. Roger, Roger. What's our vector Victor?"

Your PA calculation looks right on to me.

Density altitude factors in the temperature, and specifically the temperature deviation from*standard* which is 15^{o} C or 59^{o}F at sea level and the standard adiabatic lapse rate of 2^{o} C per thousand feet of elevation. The standard temperature for TEX should be something like -3^{o} C so if it is warmer than that, the DA is higher than airport elevation, if it is colder than that the DA is lower.

I used to have a formula for this. I found that I never needed it, however, as most larger aircraft have performance charts that find it for themselves. That is, you might enter the chart at your pressure altitude, go across to the temperature and read your solution.

Density altitude factors in the temperature, and specifically the temperature deviation from

I used to have a formula for this. I found that I never needed it, however, as most larger aircraft have performance charts that find it for themselves. That is, you might enter the chart at your pressure altitude, go across to the temperature and read your solution.

Happiness is not seeing another trite Ste. Maarten photo all week long.

Calculating them might be tough, but what they are is simple enough. There's something called the International Standard Atmosphere, a model that specifies what the temperature, pressure and density are at any given altitude on a "Standard Day". Note that they're not independent; if the temperature is 15 C and the pressure is 1013.25 millibars (the Standard sea-level values) then the density has to be Standard too.

So, density altitude is simply the altitude that (on a Standard Day) has the density that you're experiencing at the moment.

If you google International Standard Atmosphere you can find calculators that give the ISA values for any altitude.

So, density altitude is simply the altitude that (on a Standard Day) has the density that you're experiencing at the moment.

If you google International Standard Atmosphere you can find calculators that give the ISA values for any altitude.

Density altitude is simply pressure altitude corrected for non standard temperature.

To figure density altitude, in your scenario, the information you are missing is the temperature at Telluride.

Many pilots that are not accustomed to flying out of high altitude airports make the mistake of thinking that it's only 70 degrees at an airport at 6500ft so that's not too bad and don't bother with figuring out airplane performance. but standard temperature at 6500ft is somewhere around 38F so you are already about 32 degrees above standard temperature and your aircraft performance is much degraded.

To figure density altitude, in your scenario, the information you are missing is the temperature at Telluride.

Many pilots that are not accustomed to flying out of high altitude airports make the mistake of thinking that it's only 70 degrees at an airport at 6500ft so that's not too bad and don't bother with figuring out airplane performance. but standard temperature at 6500ft is somewhere around 38F so you are already about 32 degrees above standard temperature and your aircraft performance is much degraded.

Bonus animus sit, ab experientia. Quod salvatum fuerit de malis usu venit judicium.

Below is a calculator for density altitude. You can play around with it and see how the different values change the result.

http://www.wahiduddin.net/calc/calc_da_em.htm

http://www.wahiduddin.net/calc/calc_da_em.htm

- Bellerophon
**Posts:**522**Joined:**

The answers given above by various posters are correct, density altitude (DA) is pressure altitude (PA) corrected for non-standard temperature.

Well, even with the altimeter setting steady on 29.87” hg, Telluride can still experience a wide variety of outside air temperatures, and these will have an effect on your aircraft’s performance that must be accounted for.

An easy rule of thumb to calculate DA from PA is this:

In order to calculate the density altitude at Telluride, we need to know the OAT, and, as you do not quote an OAT, let us assume that this is -11°C in Winter and +29°C in Summer.

At an elevation of 9,078ft, the ISA temperature at Telluride should be -3°C, and you have already calculated correctly that at an altimeter setting of 29.87” hg, the PA is 9,128ft.

In the Winter case, the temperature deviation is -8°C below ISA, so we should subtract 1,000ft from the PA of 9,128ft, to give a DA of 8,128ft.

In the Summer case, the temperature deviation is +32°C above ISA, so we should add 4,000ft to the PA of 9,128ft, to give a DA of 13,128ft.

A variation in DA of 5,000ft, at the same airfield, at the same altimeter setting, just because the temperature changed! You can see why pilots of all aircraft types need to exercise great care when operating out of hot and high airfields.

Regards

Bellerophon

The forumla I'm familiar with:

DA = PA + 120 * (ISA Deviation)

where...

DA = Density Altitude

PA = Pressure Altitude

ISA Deviation in degees C

This formula seems to fit closely with the 8 degrees / 1000 feet rule of thumb above.

DA = PA + 120 * (ISA Deviation)

where...

DA = Density Altitude

PA = Pressure Altitude

ISA Deviation in degees C

This formula seems to fit closely with the 8 degrees / 1000 feet rule of thumb above.

Thanks for all the good posts. From using the density altitude calculator I figured out that a summer day of 68 degrees in Telluride would give a density altitude of over 12000 ft!

"We have clearance Clarence. Roger, Roger. What's our vector Victor?"

Let's use KISS method (Keep it Simple Stupid)

Altitude (correct for non std pressure ) ===> Pressure Alt (correct it for non std. temperature ) ====> Density Altitude.

There is also the factor of humidity that comes into play in density altitude, but that's negligible.

Hope this helps..

Altitude (correct for non std pressure ) ===> Pressure Alt (correct it for non std. temperature ) ====> Density Altitude.

There is also the factor of humidity that comes into play in density altitude, but that's negligible.

Hope this helps..

Earthbound misfit I

I saw that relative humidity factor in the calculator and I've heard other people whom I respect talk about it, but I'd like to know exactly how humidity affects DA. Not "why" as I understand that humid air is less dense, but, numerically - how?

I've written manuals for, flown, instructed on, or consulted in flight ops on A-320, A-330, B-727, B-737, B-757, B-767, BAe-146, DC-3, DC-9 and MD-80 as well as turboprops at half a dozen airlines and I have never once seen a performance chart that had an entry for humidity.

I believe strongly in getting to know the performance charts that are available for your airplane. I once taught an ATP written exam prep course and had two students in this class. One was a fifty-something businessman who owned a C-421 and the other student was a U-2 pilot.

Normally you kind of teach to the middle of the class. In this case there was no middle! The businessman had never once in twenty years with a license so much as looked at the performance charts for one of his airplanes. The U-2 pilot was an instructor pilot in his plane and lived (or died) with those charts. Fortunately he was sharp enough to get what I was teaching him, and still have time and neurons left over to help the other student or we'd have never gotten through the subject.

Still I would bet that the businessman never worked up the nerve to take the test. He probably just continues to stuff his plane full of people and bags and skis and head for the high elevation airports around the west.

I've written manuals for, flown, instructed on, or consulted in flight ops on A-320, A-330, B-727, B-737, B-757, B-767, BAe-146, DC-3, DC-9 and MD-80 as well as turboprops at half a dozen airlines and I have never once seen a performance chart that had an entry for humidity.

I believe strongly in getting to know the performance charts that are available for your airplane. I once taught an ATP written exam prep course and had two students in this class. One was a fifty-something businessman who owned a C-421 and the other student was a U-2 pilot.

Normally you kind of teach to the middle of the class. In this case there was no middle! The businessman had never once in twenty years with a license so much as looked at the performance charts for one of his airplanes. The U-2 pilot was an instructor pilot in his plane and lived (or died) with those charts. Fortunately he was sharp enough to get what I was teaching him, and still have time and neurons left over to help the other student or we'd have never gotten through the subject.

Still I would bet that the businessman never worked up the nerve to take the test. He probably just continues to stuff his plane full of people and bags and skis and head for the high elevation airports around the west.

Happiness is not seeing another trite Ste. Maarten photo all week long.

SlamClick, you're looking at a roughly 500-1000ft increase in density altitude when going from perfectly dry air to saturated air when air temp is around 100 degrees F. When it is around 30 degrees F, the increase is less than 100ft (as there is obviously much less moisture that the air can hold).

So, I'd say that humidity varies density altitude on the same order as pressure variances do. Why don't we compute it when figuring density altitude? Simply...its hard. As you can see from above, density altitude variations not only depend on the humidity, but also the air temperature. Doing it based off of dewpoint would not be as bad, but still more complicated and more intense than makers of density altitude charts care to do.

So, I'd say that humidity varies density altitude on the same order as pressure variances do. Why don't we compute it when figuring density altitude? Simply...its hard. As you can see from above, density altitude variations not only depend on the humidity, but also the air temperature. Doing it based off of dewpoint would not be as bad, but still more complicated and more intense than makers of density altitude charts care to do.

I'm no expert, but you'd think we could get a pretty good idea of humid air density from a steam table.

At 15 Celsius, water's vapor pressure is 17.1 millibars (says the steam table)-- so at 100% humidity at 15 C, the air pressure is 17.1 millibars less than the total pressure, and at 50% humidity it's 8.55 millibars less-- right? Water vapor is said to be 62.2% as dense as air, so seems like we should be able to work it out.

At 15 Celsius, water's vapor pressure is 17.1 millibars (says the steam table)-- so at 100% humidity at 15 C, the air pressure is 17.1 millibars less than the total pressure, and at 50% humidity it's 8.55 millibars less-- right? Water vapor is said to be 62.2% as dense as air, so seems like we should be able to work it out.

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