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

[@sheikhsami9300]

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]

It means a lot sir. Thanks for your comment ☺️

[@Sych.]

This is an awesome channel!

[@shauzinsyeda9714]

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

[@aviationalphabet6193]

Thanks for watching ❤️☺️

[@alpha_4201]

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

[@aviationalphabet6193]

Thanks a lot for the support ☺️

[@janu5853]

Bro your videos useful Tq bro

[@md.hasibulhassan4054]

Thank you

[@justinseagull5884]

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

[@aviationalphabet6193]

Thanks for watching....keep supporting ❤️

[@lynnchidz]

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]

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

[@Vishal-pg4zo]

Thank you sir

[@charanbasireddy5755]

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

[@aviationalphabet6193]

It means a lot ☺️

[@shahriarsanto7729]

Thanks you 🙏 very much brother 💕💕

[@aviationalphabet6193]

It means a lot to me brother 😊

[@hemvrm]

Informative 🔥

[@aviationalphabet6193]

Thanks a lot ☺️

[@hemvrm]

@@aviationalphabet6193 do cover other concepts aswell

[@aviationalphabet6193]

@@hemvrm will try my best

[@kjchethankumar7536]

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

[@aviationalphabet6193]

It's practically not possible for me dude 😅

[@mr.godbole6832]

Thank you for video

[@aviationalphabet6193]

Thanks a lot for watching 😊

[@UCxDarkSoul]

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

[@shravankadam9866]

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

[@vikascharan5431]

#kcpd🌋

[@muhammadibraheem2850]

how to derive these equations?

[@aviationalphabet6193]

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...

[@arabes3554]

hello. where did you get the 2.72? 20:00

[@tech2travel41]

The value of e is 2.72

[@arabes3554]

can you elaborate more sir where 2,72 get ?

[@sarandicarlomichael2109]

e is constant

[@nms2294]

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]

Pls repley🙂

[@aviationalphabet6193]

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

[@user-uz1vu9lo8h]

anybody having an exam tomorrow