I've studied this, had lectures on this, but by far, this is the best explanation with fantastic slides on this topic. I watched it on the big screen while taking notes in my "important facts" little note book, I'm filling over the years.
Nice. Just a small correction: the pitot tube doesn't measure the dynamic pressure. It measures the TOTAL PRESSURE and ultimately DEDUCES the dynamic pressure from it, by subtracting the static pressure part (obtained from the static port)
The Pitot Tube doesn't actually measure anything if we are being pedantic. The PT is an inlet which allows the flow of both Dynamic Pressure and Static Pressure to the instrument. Once in teh instrument, the Dynamic and Static pressure from the Pitot Tube are met with the Static Pressure from teh Static Pressure source and the calibrated equipment returns a value to the reading card on the instrument.....
There is a free Apps for the EB6 you can use on your iPad, phone and Mac. Tyler can you provide any info on the Apps you use? By the way the videos are very professional and informative, keep up the good work.
Hi sir if mach speed is 0.78 & OAT is -28*c @ FL 240, then magnetic course of plane is 260* True wind 280*, mag variation 11*E, magnetic wind 269*, Wind speed 50 kts, Distance of leg 93.3 nm. So what's the true airspeed, Ground speed, & time of the leg *How to do with manual calculation without CX-3?
Beyond The Stars Because EASA say so. You're not always given all the information you require to answer a question. So regardless of whether you're asked to calculate it directly, you may need to.
your plane speed increases by about 2% per 1000 feet due to less air resistance ,, but what it says on the instrument inside the plane stays the same .. so you need to know both speeds to calculate how much time it takes to get some where and what speed to fly the plane at
Really excellent presentation. I've learned alot thanks to your straightforward explanation. It is a tricky instrument to get to grips with, but practicing each stage often helps to make it easier to read.
actually, IAS is proportional to the difference between total pressure (pitot tube) and static pressure (static ports)! and the velocity of the dynamic pressure is the true airspeed ONLY for Mach
yep, moreless under 180kias and above 18000ft, this were the agreed limits to start to consider the fluid compressible, at least when I took my exams some years ago
I've studied this, had lectures on this, but by far, this is the best explanation with fantastic slides on this topic. I watched it on the big screen while taking notes in my "important facts" little note book, I'm filling over the years.
Glad you enjoyed it. Thank you for the comment.
The best CRP-5 related explanations by far 🌟🌟🌟🌟🌟👍
A well thought-out and very clearly presented video. Many thanks for your hard work.
☺️
Very useful, added more depth to my understanding of the principle.
great video, studying for my aircraft engineer licence aerodynamics module 8 and this really helps my understanding of airspeed.
Nice. Just a small correction: the pitot tube doesn't measure the dynamic pressure. It measures the TOTAL PRESSURE and ultimately DEDUCES the dynamic pressure from it, by subtracting the static pressure part (obtained from the static port)
Good point, thank you
The Pitot Tube doesn't actually measure anything if we are being pedantic. The PT is an inlet which allows the flow of both Dynamic Pressure and Static Pressure to the instrument. Once in teh instrument, the Dynamic and Static pressure from the Pitot Tube are met with the Static Pressure from teh Static Pressure source and the calibrated equipment returns a value to the reading card on the instrument.....
Great Video it tuck me while but i got it right in the end. Thank you for this video mate
Quite flattering to see my notes being used.
how can someone dislike a video such this!!!! grats.. nice video
Really really well done!!!
So very helpful. Hopefully you become an instructor one day
There is a free Apps for the EB6 you can use on your iPad, phone and Mac. Tyler can you provide any info on the Apps you use?
By the way the videos are very professional and informative, keep up the good work.
taking my written in 1 week!! thank you :)
Great video, where can I get aCRP-5 for my computer like the one you have in the video?
I want to know it as well ;) ;) It is awesome :-)
I found only this: www.e6bx.com/e6b/ But it is not as that pretty :-/
Hi sir if mach speed is 0.78 & OAT is -28*c @ FL 240, then magnetic course of plane is 260* True wind 280*, mag variation 11*E, magnetic wind 269*, Wind speed 50 kts, Distance of leg 93.3 nm.
So what's the true airspeed, Ground speed, & time of the leg
*How to do with manual calculation without CX-3?
Thanks for the great tutorial.
just add 2 % per 1000 feet onto your IAS to get your TAS :))
And what with temperature correction?
For example I have FL120 IAS 200 OAT -5
So using your formula TAS is 248 kt.
Correct is 242 - Too much diffrent
Thanks, this helped me :)
very good job!
thank you!
Very helpful thanks
Thanks a lot man..
My CRP is slowly starting to look a lot less like a jumble of numbers and is slowly starting to mean something haha
Some minor errors.. but close enough
Why do i even need to calculate???
Beyond The Stars Because EASA say so. You're not always given all the information you require to answer a question. So regardless of whether you're asked to calculate it directly, you may need to.
oh ok , this the calculate for airline pilots only? or even private pilots?
Beyond The Stars It's mainly for the EASA ATPL theory exams that are required to be sat before commencing a CPL.
duh it looks a bit difficult to me , i am not good at maths
your plane speed increases by about 2% per 1000 feet due to less air resistance ,, but what it says on the instrument inside the plane stays the same .. so you need to know both speeds to calculate how much time it takes to get some where and what speed to fly the plane at
These videos are very useful, keep the good work up!
Really excellent presentation. I've learned alot thanks to your straightforward explanation. It is a tricky instrument to get to grips with, but practicing each stage often helps to make it easier to read.
Hi
Which chart do use about CRPS website ?
It will be very useful for me to training from the website
Don't watch this mess. There are other, more easily explained videos. No pilot cares about the math at the pitot tube. EVER.
actually, IAS is proportional to the difference between total pressure (pitot tube) and static pressure (static ports)! and the velocity of the dynamic pressure is the true airspeed ONLY for Mach
yep, moreless under 180kias and above 18000ft, this were the agreed limits to start to consider the fluid compressible, at least when I took my exams some years ago
Excellent explanation, thank you
Problem is my instrument is labeled different
Nice thanks for sharing your video.
Great tutorial,
All of those stuffs are good.....But i think u have a problem on ur tounge
Any Video about CR-3. How to find TAS from a given CAS and FL using CR-3
Brilliant - many thanks. 🙏
It’s excellent explanation thanks
The cr5 video starts -> 13:28
bravo!
its a piper warrior
what is?
Going for my ppl/h... navigation... very helpful.... cheers
Thank You mate for that video! Perfect explenation for me! :D