International Standard Atmosphere |Temperature Pressure Density variation with altitude

International Standard Atmosphere |Temperature Pressure Density variation with altitude | problems

Рет қаралды 10,998

2 жыл бұрын

Пікірлер: 39

@sheikhsami9300 2 ай бұрын

It was really very much helpful for my CT exam . I was not clear about the topic but now I am fully clear . Thanks a lot .

@aviationalphabet6193 2 ай бұрын

It means a lot sir. Thanks for your comment ☺️

@Sych. Ай бұрын

This is an awesome channel!

@alpha_4201 Жыл бұрын

New subscriber here. Looking forward for this channel to grow.

@aviationalphabet6193 Жыл бұрын

Thanks a lot for the support ☺️

@shauzinsyeda9714 10 ай бұрын

Your explanation is very clear and excellent! Thank you very much!

@aviationalphabet6193 10 ай бұрын

Thanks for watching ❤️☺️

@lynnchidz 8 ай бұрын

I just found this video and thank you so much for the explanation. But what if you're already given that T=15-0.0065h for Toussaint's formula and supposed to find the pressure at geopotential altitude 5km

@tsehayenegash8394 Жыл бұрын

Nice video. I have a few questions. I have 15 years radiosonde temperature data. How can I determine lapse rate tropopause temperature and lapse rate tropopause height by using this data? thank you

@md.hasibulhassan4054 2 ай бұрын

Thank you

@janu5853 Жыл бұрын

Bro your videos useful Tq bro

@Vishal-pg4zo Жыл бұрын

Thank you sir

@hemvrm 2 жыл бұрын

Informative 🔥

@aviationalphabet6193 2 жыл бұрын

Thanks a lot ☺️

@hemvrm 2 жыл бұрын

@@aviationalphabet6193 do cover other concepts aswell

@aviationalphabet6193 2 жыл бұрын

@@hemvrm will try my best

@kjchethankumar7536 2 жыл бұрын

Awesome work...😄 Waiting for control theory....🙂

@aviationalphabet6193 2 жыл бұрын

It's practically not possible for me dude 😅

@charanbasireddy 2 жыл бұрын

I saw this video before exam and scored maximum thanks sir for information 🫂

@aviationalphabet6193 2 жыл бұрын

It means a lot ☺️

@justinseagull5884 9 ай бұрын

Thank you so much... It was so helpful ♡

@aviationalphabet6193 9 ай бұрын

Thanks for watching....keep supporting ❤️

@UCxDarkSoul 3 ай бұрын

How to find pressure temperature and density when the altitude is given as 61000m

@shravankadam9866 Ай бұрын

P1/P0=t1/t2)^-(g0/aR)

@mr.godbole6832 2 жыл бұрын

Thank you for video

@aviationalphabet6193 2 жыл бұрын

Thanks a lot for watching 😊

@shahriarsanto7729 10 ай бұрын

Thanks you 🙏 very much brother 💕💕

@aviationalphabet6193 10 ай бұрын

It means a lot to me brother 😊

@vikascharan5431 2 жыл бұрын

#kcpd🌋

@muhammadibraheem2850 Жыл бұрын

how to derive these equations?

@aviationalphabet6193 Жыл бұрын

There is a course in edx platform for free named as "'Introduction to aeronautical engineering". You can get these derivations in that course. You can go through it...

@nms2294 11 ай бұрын

Calculate the ambient temperature at an altitude of 15 km over a city, which has ISA+15 atmosphere. Bro how this type questions are answered if ISA deviation values are given

@nms2294 11 ай бұрын

Pls repley🙂

@aviationalphabet6193 11 ай бұрын

You can use those values which are given in the question...