Airspeed in cooler air
 

Hi, I was wondering if someone could help me brush up airspeed changes when flying inside air masses of different temperature. For example how does IAS and TAS change when flying into cooler mass of air ?

Thanks !

As I see it..
flying into a cooler air, more air molecules present in the air.
Pitot tube will sense a higher volume of molecules, hence will show a higher IAS.
On the other hand, more molecules will cause a higher drag, hence true speed will be lower.

The IAS-TAS relationship with a change in temp at a constant alt is easily solved using the CRP5 or suchlike.

What IAS you will see for a constant tq or N1 setting with a change of temp is difficult to say, will guess that a look at the aircrafts manual will reveal that.

Econ Crz, or whatever you choose to fly, is a fixed IAS. e.g. 250 kts or M.78.
In warmer air the TAS will be higher than in cooler air. At ISA +10 you will fly faster than at ISA -10.
In still air, your flight time can vary by several minutes an hour under such circumstances.

Thanks guys ! :ok: