Thrust Is provided By ? A. Rate of change of momentum of air B. Change in Mass flow rate
@AliyaBurkit
3 жыл бұрын
A
@prashantrao8040
3 жыл бұрын
@@AliyaBurkit but mam....if we change rate of mass flow ....then also must change in thrust of aircraft
@batuhan3066
3 жыл бұрын
mass flow rate does not change through the engine thus, it's not changed thrust or create thrust(it is kinda tools for create thrust). if u assigned a new mass flow rate your thrust will be changing but the reason for that is changing the momentum of air.
@prashantrao8040
2 жыл бұрын
@@batuhan3066 yeh brthr u r right
@lokeshcheemala5064
2 жыл бұрын
Thanks for explanation mam....
@derjoh1986
Жыл бұрын
I don't understand half of what you're saying regarding this but thank you for being part of the evolution of aeronautics. People like you that makes America so great.
@misbahulzannatfabiha9458
3 жыл бұрын
Hi Aliya! PLEASEEE keep making Aircraft Propulsion videos, I am struggling with my Propulsion course this semester. It's very motivating to hear from a fellow woman in Aerospace engineering. This pushed me to work harder. I love your explanations, keep it up!!
@Vishnu00011
3 жыл бұрын
first comment your channel is best love from india!!
@AliyaBurkit
3 жыл бұрын
Thank you for being a subscriber!
@EmersondeOliveira
2 жыл бұрын
Simple answer and accessible to the general public. Congratulations!
@MehediHasan-ow3gc
3 жыл бұрын
You explain very well. Love from Bangladesh ❤️
@AliyaBurkit
3 жыл бұрын
Thank you for watching!
@yato2557
3 жыл бұрын
Finally propulsion letsgooo!!! Madam please teach all of it including compressors and turbines Thankyou !🙏🏻
@AliyaBurkit
3 жыл бұрын
Haha, moving on. Thank you for watching!
@nurababajada7024
3 жыл бұрын
I was reluctant in studyng Aerospace engineering b4 watchng ur videos, but now i feel like an aerodynamic guru, thanks to ur videos.
@AliyaBurkit
3 жыл бұрын
Thank you, but there is still so much more to aerodynamics 😅
@orbitronsfs404
3 жыл бұрын
I have subscribed because 1) You explain everything very well and understandable for people like me who are new to learning aerospace and 2) You have a masters degree in Aerospace Engineering so you know what your talking about! PERFECT
@AliyaBurkit
3 жыл бұрын
Thank you so much!
@luisbispo212
3 жыл бұрын
This channel is incredible. The way you explain it is really great. Love from Brazil ❤️🛫✈
@AliyaBurkit
3 жыл бұрын
Thank you so much!
@BenjaminOrthodox
3 жыл бұрын
This channel is a gift! haha
@copycat3410
3 жыл бұрын
Your hard work is more than the views and subscriber you get 😭😭 sad. keep growing love from india
@AliyaBurkit
3 жыл бұрын
Thank you so much! Will keep going 💪
@rubangiramartin
Жыл бұрын
Thanks alot Engineer, I will learn a lot from you. So far so good
@chrismachabee3128
2 жыл бұрын
Thank you. It is not easy to understand. I have look at those equations so much and mot been able to understand. Your explanation was very good. I would only ask one thing for the future and that is, that after your expalnation you can use real number coupled with a real jet engine. I think that would increase my understand and help me remember the equation if I see it actually used showing a real real. just an idea, Thank you Master Aliya.
@danielrizzo4927
2 жыл бұрын
Thank you!
@jiaaggarwal5873
Жыл бұрын
your videos are amazing, thank you so much!! please keep making more videos relating to aerospace engineering, very interesting content
@jatintrivedi5632
21 күн бұрын
Hello beautifil Aaliyaji Burkt, You missed out on accounting gravity resistance and air resistance experienced during lift off.
@engineers_hub
7 ай бұрын
Hi, thanks for the video. can you demonstrate how to incorporate the fluid mass in the equation? Will the mass of the fluid be inlet or outlet and which velocity do you use it with to get its momentum?
@easyaeronautics8554
3 жыл бұрын
First o will get ur help when i will doing mu aerospace graduation. Love u..as friend😀
@AliyaBurkit
3 жыл бұрын
Great 👍
@siphesihleyende8390
3 жыл бұрын
you are awesome please continue making more videos. definitely killing that ATG exam with this
@marcoreale02
3 жыл бұрын
Thank you so much this video explains everything in a much more clear way compared to others!!
@AliyaBurkit
3 жыл бұрын
I'm so glad!
@sanjitkumarsen1474
3 жыл бұрын
Your lectures are very lucid and elaborate. Please explain calculation of required thrust for particular airframe. I am from India
@anbu3964
3 жыл бұрын
Hello mam , I am anbu studying ame . Your videos use full me very much. I appreciate you. Keep doing well. I am also from India.
@AliyaBurkit
3 жыл бұрын
Glad to help!
@vikrantloyare8576
3 жыл бұрын
We love u man! Especially ur lectures.
@AliyaBurkit
3 жыл бұрын
Thanks for watching!
@vikrampawar8400
2 жыл бұрын
Hi, your video are very good for understanding.
@arjunnarayanan5474
3 жыл бұрын
great tutorial thanks
@AliyaBurkit
3 жыл бұрын
Glad to help
@lionelnishan5623
2 жыл бұрын
Nicely Explained !!!
@yosoyroman875
Жыл бұрын
Here I was just trying to learn how to calculate thrust 😮and I was treated to a roller coaster of emotions too
@astrogabba1190
2 жыл бұрын
2:24 there's a mistake, in the combustion chamber the pressure DOES NOT rise. Maximum pressure in a turbojet (or turbofan) is reached at the outlet of the compressor just before entering the combustion chamber. You can simply verify this by looking at the Brayton cycle. In reality Into the combustion chamber the pressure actually decreases a little bit because of Rayleigh losses.
@_boss_mafia_
3 жыл бұрын
love from sri lanka teacher
@AliyaBurkit
3 жыл бұрын
Thanks :)
@_boss_mafia_
3 жыл бұрын
thanks for u teacher not for us u done a great job
@NoRecentActivityFound
3 жыл бұрын
Thank you !! 🙂🙂
@AliyaBurkit
3 жыл бұрын
Welcome!
@feyselmussema1619
3 жыл бұрын
hello can u make a video on how to drive general GTE formula
@feyselmussema1619
3 жыл бұрын
hello can u make a video on how to drive general GTE formula
@asdf9510ify
3 жыл бұрын
Wow. So SImple. Hopefully you do become a Good Professor
@AliyaBurkit
3 жыл бұрын
Haha thanks, that's not my goal 😅
@shoubhikpal3460
3 жыл бұрын
Favourite ❤️.....which country u belong?...I want to know.....and a QnA video we want
@Vagrantbackpacker
3 жыл бұрын
Thanks shoubhik for recommending this channel....loved it
@DecodeWithPal
3 жыл бұрын
Thanks shoubhik for recommending this channel....Aliya u are making awesome videos keep going...
@shoubhikpal3460
3 жыл бұрын
Thank u guys.... support her.....she is really awesome ❤️
@AliyaBurkit
3 жыл бұрын
I'm from Kazakhstan
@AliyaBurkit
3 жыл бұрын
Thank you for joining!
@spaceengineering6529
2 жыл бұрын
Why is the direction of P2Ae opposite the direction of air flow?
@albertom7776
3 жыл бұрын
thanks, but in the combustion chamber the pressure remains constant (in ideal cases), in the reality the pressure drops.
@meghaRandome
Жыл бұрын
what are the casual parameters for the fuel flow ??
@joneginnesh2748
3 жыл бұрын
Thank you Mam
@AliyaBurkit
3 жыл бұрын
Most welcome 😊
@IronDragonGroup
3 жыл бұрын
Wonderful video, certainly helped me to better understand the forces acting within a jet engine. Is there a way to calculate the thrust using the temperature of combustion though? I am building a mini turbojet, and the only variable I know for sure is the combustion temperature. Thank you!
@LordBagdanoff
2 жыл бұрын
Why is the units for thrust pound force lbf?
@rashmiamahanaz937
2 жыл бұрын
Sis can you tell..is aviation management subject is good for build up caree?..
@AirlinesDisasterAnalysis
3 жыл бұрын
Thanks Alia
@AliyaBurkit
3 жыл бұрын
Thanks for watching!
@AirlinesDisasterAnalysis
3 жыл бұрын
Your explanation was so vivid, I just can't wait when next one wil come..Stay safe n sound.
@AliyaBurkit
3 жыл бұрын
Thanks for watching! Next one is coming
@KP_Wellness
3 жыл бұрын
can u explain about hang glider lift. please. I want to understand it properly. no one can teach me better than u. I wish u could be my teacher.
@copycat3410
3 жыл бұрын
Here also an Indian
@francescosaltarel2551
3 жыл бұрын
Great explanation👍🏻 A question: would be the heating of the gasses after the turbine (not with afterburner) generate more thrust?
@AliyaBurkit
3 жыл бұрын
Great question. No, thrust only depends on how much air and how fast it's leaving the engine. You can't make more air by heating it up
@francescosaltarel2551
3 жыл бұрын
@@AliyaBurkit thank you so much This is right😅😂 Thank you😉
@worldofstrings
Жыл бұрын
Aliya I'm trying my best to figure out those equations, how does the weight factor which has to with gravity fits into the equations?
@tung6364
3 жыл бұрын
help me !!! How to calculate thrust of a jet engine through RPM
@KP_Wellness
3 жыл бұрын
please upload newtons third law on lift fast
@AliyaBurkit
3 жыл бұрын
kzitem.info/news/bejne/s62ElmSkkqyrqYI
@sumanthchandra.d9208
3 жыл бұрын
Hi aliya ....is possible can u make video about Inertia propulsion and scope as well as limitations...
@bakhabar9059
2 жыл бұрын
please send me your WhatsApp number or cell number. i will contact you
@ANMOLKUMAR-es4pv
3 жыл бұрын
Hi Aliya, you explain very nice. Aerospace always fascinate me. thanks for wonderful video. you wear NASA- tshirts . have you worked in nasa projects ?
@AliyaBurkit
3 жыл бұрын
Thank you for watching! No, it's still my dream))
@knowledgeispower7738
3 жыл бұрын
THANKS A LOT TEACHER YOU TEACH BEAUTIFUL ❤️👍
@AliyaBurkit
3 жыл бұрын
Thank you!
@Lucy-gs5rm
3 жыл бұрын
Hi! Do you maybe have a practice example for this equation?
@AliyaBurkit
3 жыл бұрын
Yes, I will have videos on solving actual problems
@karthikc8758
3 жыл бұрын
What specialization have you done in aerospace engineering master's? Ma'am
@mgsearch7352
2 жыл бұрын
Nice explanation, but it's better to have an example. Thanks
@mubassirjavadjavad1696
3 жыл бұрын
Madoum, is aerospace engineering a good profession I have 99 % in both physics and mathematics. Can i become a e
@OYEUAV
2 жыл бұрын
Please ma'am... When are you doing your next video.... It been a while
@DMGInfinityWarrior
3 жыл бұрын
i understand the continuity equations regarding the mass flow rate, but how are both values of m-dot the same if the exit velocity is increased and air is compressed increasing the velocity?
@DMGInfinityWarrior
3 жыл бұрын
*if the engine has a centrifuge
@0623kaboom
2 жыл бұрын
so IF i have a 65,000 lb plane ... with 2 engines that generate 22,000 lbs of thrust each ....then my thrust of 44,000= mdot(v2-v1)+p2Ae-p1Ai .if I understood that correctly ... how does one find out how FAST this plane could go ... from here
@0623kaboom
2 жыл бұрын
of all the video's i have watched this is actually the first one that is clear and concise ... yeah I subbed because of it ... now to see if I can find the answer to my question in your video's ... or even even recognise the video that my answer might be covered in lol
@aishwaryameti5308
11 ай бұрын
Hi sis Iam Aishwarya, 4th year Aerospace engineering student , I want to connect with u, how can I connect with u?
@rosishkatuwal5677
3 жыл бұрын
You look pretty as always..
@AliyaBurkit
3 жыл бұрын
Wow, thank you!
@rosishkatuwal5677
3 жыл бұрын
@@AliyaBurkit Welcome..😍😍
@John.Doe.2025
3 жыл бұрын
Мастер дегри, всё круто, все дела, но почему давление в камере сгорания растёт? Это самая большая ошибка новичков, давление после компрессора всегда падает. Об этом пишут во всех книгах.
@AliyaBurkit
3 жыл бұрын
Зачем тогда компрессор? Давление падает после сгорания, когда уходит дальше
@John.Doe.2025
3 жыл бұрын
@@AliyaBurkit Чем больше хотим выделить энергии с горючего, тем больше его надо сжечь; чтоб больше его жечь надо больше окислителя (воздуха); чтоб больше воздуха поступало надо либо увеличить трубу(двигатель) до гигантских размеров, либо поставить механизм сжатия воздуха, тогда размер двигателя будет приемлемым. Чем лучше компрессор - тем больше топлива можем сжечь и получить больше тяги при малых геометрических размерах двигателя. Камера сгорания или жаровая труба имеют выход в сторону турбины, такого сечения, чтобы при горении давление не превысило значение после диффузора компрессора. Если давление в камере сгорания превысит давление на выходе компрессора произойдёт помпаж (surge) двигателя.
@அரசியல்பொக்கிஷம்
3 жыл бұрын
Hi! Buddy .I'm a aeronautical engineering student from India. I need your support to learn the things effectively. Shall we discuss?
@eyesvewsshorts7316
2 жыл бұрын
Mam are you American🇺🇸
@petergriffin383
3 жыл бұрын
Wow what a smart elegant beautiful woman... I wish I could meet a woman as educated and talented she is. I could learn from her.
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