✅ Difference Between IAS CAS EAS TAS GS MACH - Airspeeds in Aviation

In this video you will learn all about the airspeeds in aviation and what is the difference between them all.
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Indicated Airspeed
Calibrated Airspeed
Equivalent Airspeed
True Airspeed
Ground Speed
Mach Number
Pitot Tube and Static Port
Total Pressure and Dynamic Pressure
Subsonic
Transonic
Supersonic
Hypersonic
Crossover Altitude switch from IAS to Mach

[@rengarajanmohan]

One the best explanation I've heard so far. Thanks

[@ATPLStudent]

Glad it was helpful!

[@bettinaboros6799]

Thank you this was very well explained! Simple and to the point

[@ATPLStudent]

I am glad it was helpful. best of luck

[@Wins-Wings]

Thanks for sharing ❤

[@ATPLStudent]

My pleasure mate

[@flotar3302]

Hi! Why the ias is the same with altitude?

[@RJ-yn2dj]

Why does the TAS start decreasing at change over altitude? thanks

[@armelmba509]

Due to temperature which decreases as altitude increases

[@liberteegalitefraternite7804]

But If you want to keep constant speed over altitude the your TAS will be increased. You have to fly faster to keep the appropriate value of lift experiencing thiner air with increasing altitude

[@flotar3302]

Hi! Why the ias is the same with altitude?

[@ATPLStudent]

Because IAS isn't actually a speed, but rather Dynamic pressure; that is the how much air if flowing into the Pitot Tube.

[@flotar3302]

@@ATPLStudent so ias will be Lower with altitude instead constant, right?