Hi, thanks for your work. I’m trying to find if you have made other videos about rockets. I saw your rocket equation one, and would love to learn more about the other equations involved, especially numerical recipes to integrate those equations in programming ( maybe Python since there are many numerical libraries available). For example, I’d like to graph a plot of a rocket lifting up from anywhere on Earth. Thanks again!
Bellissimo video insieme agli altri due. Veramente intetessante com una chiara edposizione per molti appassionati e studiosi dell volo spazisle. Spero che presto pubblichi molti altriv vifeo e sopratutto data la sua conoscienzs nella scienza spaziale possa introdurre un corso completo di Meccanica del volo.spaziale " che penso intetessera numerosi appassionati. Grazie e buon lavoro
First of all. I love your videos mam, @Aliya Burkit . They've been great. Thank you very much. Second of all, mam, I have two questions. First, which one of the mdot x ve and (pe-po)Ae contributes more to the rocket thrust? Second, How do rockets controls the difference in the pressure (Pe-Po)? Is it by varying the rpm of the turbopump?
The term that contributes the most to the rocket thrust is mdote*ve, also know as impulsive thrust. The second term is controlled by the shape of the nozzle, that to maximize thrust should be able to provide the same pressure of the exhaust than that of the environment. The throttle changes the speed of the exhaust only
Well, it depends which level of aerodynamics you want to understand. If it's pretty introductory, you could be fine just knowing integrals and derivatives, but if you want to dig deeper into Navier-Stokes and vortices, it gets pretty complicated. You would need to learn about multiple variable calculus, and computational fluid dynamics.
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In this video we talk about the rocket thrust equation and how it is derived from a general thrust equation.
love from sri lanka donot stop teacher go ahead
nice
It was a wonderful video. Please keep making such types of videos It helps us a lot.❤👍
Thank you
Wonderful how such a complicated topic can be explained in such a way as to make it look easy . . . A great lesson. Thank you 👍👍
Thank you for feedback!
You're such an awesome fellow, I get so eased up when i watch your videos after class. Its really demystifying. Lots of love ❤ Aliya
- Odi, Nigeria
PERFECT VIDEO.....THANK U ALIYA
You're welcome!
Your videos are so interesting! Well Done 😁
Thank you!
Hi, thanks for your work. I’m trying to find if you have made other videos about rockets. I saw your rocket equation one, and would love to learn more about the other equations involved, especially numerical recipes to integrate those equations in programming ( maybe Python since there are many numerical libraries available). For example, I’d like to graph a plot of a rocket lifting up from anywhere on Earth. Thanks again!
Thank u ma'am
You're welcome!
Your videos are soooo helpful ⛔️⛔️⛔️⛔️please keep doing videos like these looking forward for more updates
Thank you so much. This video was very helpful to understand the thrust equation in rocket science 👍🤍..
thank you, i was confuesed because sombody else called it v2 but there was no v1. now it makes sense :)
Bellissimo video insieme agli altri due. Veramente intetessante com una chiara edposizione per molti appassionati e studiosi dell volo spazisle. Spero che presto pubblichi molti altriv vifeo e sopratutto data la sua conoscienzs nella scienza spaziale possa introdurre un corso completo di Meccanica del volo.spaziale " che penso intetessera numerosi appassionati. Grazie e buon lavoro
Very nice, you deserve more subscribers
Thank you
Good video, I like, Greetings from Perú !!
thanks for studying
First of all. I love your videos mam, @Aliya Burkit . They've been great. Thank you very much.
Second of all, mam, I have two questions. First, which one of the mdot x ve and (pe-po)Ae contributes more to the rocket thrust? Second, How do rockets controls the difference in the pressure (Pe-Po)? Is it by varying the rpm of the turbopump?
The term that contributes the most to the rocket thrust is mdote*ve, also know as impulsive thrust. The second term is controlled by the shape of the nozzle, that to maximize thrust should be able to provide the same pressure of the exhaust than that of the environment. The throttle changes the speed of the exhaust only
An example along with the calculation would help me better understanding it
Just Perfect
What's the minimum TWR for any rocket to lift off the ground and go up 100 meters???
Nice explanation teacher 🎉could you please help me out which essential maths topics are needed to get a nice Clarity in this topic. Do tell......
You need to know what rate of change means, areas, and vectors. And the other topics are physics ones 😅
@@AliyaBurkit okay 👍.... thanks for replying....
wonderful video mam
As we go higher in space Po is going to decrease. So Po is not constant, is it?
Please answer somebody the thrust on rocket is in which direction of rocket
Mam , I want to know , why centre of gravity of an aircraft is at (approximately) aerodynamic centre ?
Hi i want to calculate of 107mm rocket pls tell me explain
Hi mam , i want vivid explanation of co efficient of lift,drag.
Thank you for your suggestion! It's on my plan
@@AliyaBurkit make it very fast. it's very use to my study.
@@anbu3964 I see
@@anbu3964 You will do well to learn some manners.
Did you major in propulsion mam?
What the math topics i need to understand aerodynamic
And source
Well, it depends which level of aerodynamics you want to understand. If it's pretty introductory, you could be fine just knowing integrals and derivatives, but if you want to dig deeper into Navier-Stokes and vortices, it gets pretty complicated. You would need to learn about multiple variable calculus, and computational fluid dynamics.
I love u
Hey Elon now that i know your little secret you better beware i'm coming!