Once again, you have such a simple way to explain the concepts! I have already take my exams and pass the AGK, Air Law and Communications. It was very helpful to watch your videos, specially those explaining the systems of the aircraft. Now I am starting on principles of flight and this video is very good. I like how you can put it in a simple and correct way. Sometimes I am concerned about you, because the COVID in India. 😔 I hope you are fine. I wish you all the good things, you really hare doing a great work with your videos.
Yes, the situation here is quite grim but I am doing good. Thank you for asking! and Thank you for your wishes. Kind words such as these do encourage me to make more videos which would be useful to people in aviation such as yourself. I wish you ALL THE BEST!
Static Pressure info is collected from ports that are flush with the surface and perpendicular to the free stream air, so that it does not vary with speed.
We could use sound and emf to help stabilize fly and help reduce weigh by anti gravity generate by new engine combine three element anti gravity, thrust, and interia change
Question: Air is flowing past the static port at >= the speed of the aircraft. Why isn't the measured pressure at the static port lower than true static pressure by Bernoulli's equation?
@@JxJAVIATION so consider a small plane flying at 5,000 feet ASL (air density about 20.48x10-4 slugs/ft3), at 150 MPH (220 ft/sec). Air moving over the static port at this speed has a higher kinetic energy than the stationary air inside the static port, thus it has to be at a relatively lower pressure outside. The Bernoulli equation predicts the pressure drop to be 0.346 PSI. How is air rushing past the static port different than blowing over a piece of paper (the paper rises) or blowing over the top of a wing?
@@aslPlayer to measure static pressure the port needs to be at right angle or perpendicular to the air flow. If the keep the port in the front or in line with the airflow we get the stagnation pressure(Total pressure), because the speed of air would have reduced to 0.
You are Welcome. Because of certain loses due to pressure and because of compression of air(Pressure Error) a correction has to be applied. Density correction is with reference to increase in altitude.
This is such a good explanation!
Thank you!! Check out my other videos as well!
Once again, you have such a simple way to explain the concepts!
I have already take my exams and pass the AGK, Air Law and Communications. It was very helpful to watch your videos, specially those explaining the systems of the aircraft. Now I am starting on principles of flight and this video is very good. I like how you can put it in a simple and correct way.
Sometimes I am concerned about you, because the COVID in India. 😔 I hope you are fine.
I wish you all the good things, you really hare doing a great work with your videos.
Yes, the situation here is quite grim but I am doing good. Thank you for asking! and Thank you for your wishes. Kind words such as these do encourage me to make more videos which would be useful to people in aviation such as yourself.
I wish you ALL THE BEST!
Thought its so boring video the explanation is very great
Glad it was helpful. Thank You!
Sir, very fine explaination, keep up the good work!
Thanks, will do!
Very useful video ✌️
Thank you! Do Check out my other videos as well!
Quite simplistically explained..
Just an addition of GROUND SPEED = TAS + W/V component
Thank you for the info!
GREAT CONTENT. PLEASE EXPLAIN ABOUT THE AIR DATA TEST SET TOO
Thanks and Noted!
How does an aircraft submit to the static pressure in the sky while it's flying?
Static Pressure info is collected from ports that are flush with the surface and perpendicular to the free stream air, so that it does not vary with speed.
We could use sound and emf to help stabilize fly and help reduce weigh by anti gravity generate by new engine combine three element anti gravity, thrust, and interia change
Interesting!
Question: Air is flowing past the static port at >= the speed of the aircraft. Why isn't the measured pressure at the static port lower than true static pressure by Bernoulli's equation?
It is because of the loses that occur in the flow due to friction and viscosity of the air
@@JxJAVIATION so consider a small plane flying at 5,000 feet ASL (air density about 20.48x10-4 slugs/ft3), at 150 MPH (220 ft/sec). Air moving over the static port at this speed has a higher kinetic energy than the stationary air inside the static port, thus it has to be at a relatively lower pressure outside. The Bernoulli equation predicts the pressure drop to be 0.346 PSI.
How is air rushing past the static port different than blowing over a piece of paper (the paper rises) or blowing over the top of a wing?
@@aslPlayer to measure static pressure the port needs to be at right angle or perpendicular to the air flow. If the keep the port in the front or in line with the airflow we get the stagnation pressure(Total pressure), because the speed of air would have reduced to 0.
great video
Thank You!!
Thank you very useful content
You are welcome!
Ty for great video but what do u mean by corrected pressure error corrected air compressibility corrected for density plz reply
You are Welcome. Because of certain loses due to pressure and because of compression of air(Pressure Error) a correction has to be applied. Density correction is with reference to increase in altitude.
@@JxJAVIATION okkay ty
We need at least 5 sensors front, up and lower wing area, and tail to calculate dynamic pressure
This is just to get a basic understanding of the speed measurement!
Is the data collected by Pitot tube reliable at any speed? Even the slowest,suppose the aircraft is taxing
Your response will be highly appreciated
The pitot does give an accurate reading at low speeds, even during taxiing on ground, as long as the tubes are not blocked!
Sir please make video on transformer, in module 3
What would be Transformer in module 3. Couldn't understand!
@@JxJAVIATION i am talking about aircraft maintenance engineering module s
Ty
Welcome!
airbus designs always make the vertical tail too big. they must think this aircraft banks sideways a lot.
maybe!
Avionics
also the pitot static system