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How Rocket Engines works? | Liquid Engines | Liquid Propulsion

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There are limitations of Solid rocket motors like Controllability, throttle ability and low burn duration and thus even with it's high thrust and shelf life, we need to rely on liquid engines in some stages. Here I've explained the working principle of liquid engines in the simplest way possible.
Partial Knowledge is dangerous, Watch the video till the end😊
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Опубликовано:

24 апр 2020

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Комментарии : 468

@rk25 3 года назад

feels proud when an Indian explains things related to space science 😄

@entertainerbanda4247 3 года назад

Ruko zara sabar karo abhi or bhi bahot se scientist honge India se.

@kwondo_22_mars 2 года назад

Oh you're still kid brother... There are much left that you have not seen.

@aarvraina1785 2 года назад

Then there comes isro 🤣🤣🤣

@shubhamsinha1330 3 года назад

😅i have to say tho he is a bit different from what comes to our mind when we think of rocket scientists . . . bro plz keep making videos full support

@ashishranjantalks 3 года назад

No doubt

@gauravpatil01 4 года назад

Rocket of spacex are reusable for that they require accurate control on combustion so they uses liquid engines. Am I correct?

@shashankjois5452 4 года назад

Yes absolutely correct

@shashankjois5452 4 года назад

Not only for combustion and also thrust control ,direction of thrust control,managing the landing site and only liquid engines can be refueled like a car solid motor is like Diwali rocket😁 so spaceX uses liquid engines,.

@ashishranjantalks 4 года назад

True but not the only reason

@shashankjois5452 4 года назад

@Dileep Kumar no, they are less expensive and easier than liquid engine.

@prabhatbharti4881 4 года назад

Hey Ashish, I only (used to ) watch your rocket science videos as I founded it very simple to understandable I make notes whenever I watch any rocketry videos and in future gonna make a rocket my self and try to make into space or edge of the space if not orbit :D ( a small rocket )ofcourse it's a long process and learning and understanding is the first step, later I started to watch all of your videos even on your Torq and torq talk channels, I try to watch every ad which comes on your videos ( mostly adds are about educational stuff ofcourse it makes sense as your channel is mostly on education and stuff ) just wanna tell you all the best all your videos are very informative to all of us, God bless you brother 👍😁

@ashishranjantalks 4 года назад

Thanks Prabhat, I'm glad you're finding my videos Useful😊

@ares1399 4 года назад

Hey im enjoying learning rocket science i was literally searching for this kind of lectures😍😍please explain how a rocket is ignited being very far away from it and types of fuel and everything you know!!!!🙏🙌

@ashishranjantalks 4 года назад

Will upload soon

@vishalk4647 4 года назад

I'm happy finally someone in India came up with something like this. I've been developing some solid motors before and now working on hybrid one but there's lack of some sources like this for young people. I really appreciate this.

@ashishranjantalks 4 года назад

you're welcome, if you want to talk about your work in solid motors we can talk

@vishalk4647 4 года назад

@@ashishranjantalks I'd love to talk about it.

@aftab2360 4 года назад

Very few youtuber can give this kind of knowledge 👌 thank you...

@ashishranjantalks 4 года назад

It's my pleasure

@sninfotainment9480 4 года назад

Now the fear of Rocket science will not be that much for subscribers???Keep up this series?More about cryogenics rocket science needs to revealed!

@ashishranjantalks 4 года назад

😊👍

@manishmohitesmailbox 4 года назад

Bcoz....In solid uncontrollable reactions goes on.... i loved the style of ur teaching...

@ashishranjantalks 4 года назад

Thanks a ton that is correct but not the perfect reson

@Adityaraj-xo1ii 3 года назад

Itni Ada Aur Grace ke saath ek scientist. Waah ji itni badi baat keh di aapne.

@ashishranjantalks 3 года назад

😊😊

@abhishekshrivastava177 4 года назад

How can one make all of this sound so simple? This is incredible stuff.

@ashishranjantalks 4 года назад

Thanks😁😁

@shashankjois5452 4 года назад

Sir vedio is very awesome😊😍😍😘 I think brightness in the room is little bit high so I can't see the board clearly😅 ,do check it once then vedio becomes Most beautiful😊

@ashishranjantalks 4 года назад

Noted

@abhishekshrivastava177 4 года назад

I think the answer of your question would be that solid fuels are more denser than liquid fuels so that would increase the mass of the rocket altogether. Quoting you "mass is the enemy of proplulsion. So this reason sounds plausible.Also,we have more control over the thrust provided by liquid engines than the solid ones,so I think this is another reason space x don't use solid engines. But again if things were this simple,I would be working in space x right now 😆

@ashishranjantalks 4 года назад

Good attempt Abhishek, I'll discuss soon

@gearxgaming4186 3 года назад

Great explainarion sir

@ashishranjantalks 2 года назад

Thanks a lot 😊

@nikhiladhav9595 4 года назад

can u decide to make a video on " how I became a space enthusiast , and when, how I decided to be an ISRO scientist ?"

@ashishranjantalks 4 года назад

yes, that's a good idea

@littlerocx 4 года назад

Good one Anna, please carry on...

@ashishranjantalks 4 года назад

Thanks sure

@atharvavadalkar6340 3 года назад

HI, I have seen your videos regarding Rocket Propulsion. They are very simple and easily understandable. I wanted to ask that can't we use Plasma particles for rocket propulsion? and Can you make videos for types of Jet Engines in Rocket Propulsion.

@ashishranjantalks 3 года назад

Will try to cover

@starshipboy6680 3 года назад

Nice vid dude, can u even make a vid explaining reaction wheels too

@ashishranjantalks 2 года назад

Will try to cover in a video

@shashankachari4825 4 года назад

Woah! Look at the flow and sequence of explanation!

@ashishranjantalks 4 года назад

Thanks😁

@rtngiri5211 3 года назад

Sir this video is awesome well basic explains ...post video which has more details in it ...explain us about the engine of spaceX rockets...

@ashishranjantalks 3 года назад

😊😊

@believer1557 4 года назад

Being a medical student i like your engineering lectures😂😂 #mathsbio students😂😂😂 Rocketscience was my love till class 10 after class 12 humanbody science become my love😉😂 By the way if u reading my comment love your video and dedication...i have been made a way long by seening your videos ..its keep me motivated 😊😊😊feeling blessed

@ashishranjantalks 4 года назад

My objective is to make arts students interested into Rocketry😊

@believer1557 4 года назад

@@ashishranjantalks thanks for reply anyways BIG FAN SIR

@ananthua8718 3 года назад

Best presentation....loved...it Very ...very easy to understand..

@ananthua8718 3 года назад

I have applied to diploma technician in LPSC ISRO. It was very much useful for me as a beginner.. thank u😊👌👌

@ashishranjantalks 3 года назад

You’re most welcome😊

@AbhishekSingh__10_ 3 года назад

Please continue with this series of rocket science, as they are one of best explanations I found 😊.....please continue it ....

@ashishranjantalks 3 года назад

Sure will 😁

@nirbhayatiwari5425 2 года назад

What ?? Everyday Astronaut explains better than him ...

@Radhe8895 4 года назад

Because solid engine have uncontrollable combustion. Rather liquid engine have controllable combustion. And so during separation they need to come back, the booster on landing site which need controllable combustion which provided by liquid engine . So called reusable booster saving a lot.

@ashishranjantalks 4 года назад

Yes very True😊👍

@vyahruthkota3437 4 года назад

Ok. Then why such reusable boosters are not used by our isro?

@Radhe8895 4 года назад

@@vyahruthkota3437 booster based on engine and it's complex, spacex failed three to do that while isro don't have attempt on that technology. Isro has lot to do like putting sattalite in orbit, chandan yan etc u can on there website for upcomming programs. so it need that government funds to private organisation so that they can work on technology.

@godsparticle7657 4 года назад

Dammn too good !!!! 😍

@ashishranjantalks 4 года назад

Thanks😊

@aktscienceandgaming7487 3 года назад

Awesome sir

@ashishranjantalks 3 года назад

😊😊

@anuprakashchoudhary439 4 года назад

Great explanation 👍🌟

@ashishranjantalks 4 года назад

Glad you think so!

@TechTalkIeorTamil 4 года назад

Sub sonic Super sonic Thrust Pump Increase velocity Mass enemy of propulsion Prime over( turbine) Rapid combustion Increase pressure Turbo pump Feed back mechanism Mixture ratio maintained Combustion increases velocity increases by increasing fuel & oxidizer by pump :turbine

@ashishranjantalks 4 года назад

🙌

@veera7391 4 года назад

Will there be a starter motor to start the turbine to pressurise fuel & oxidiser Initially (before actual combustion starts) in the beginning??????????!

@ashishranjantalks 4 года назад

not necessarily

@shubhamsinha1330 3 года назад

sir can you plz make a dedicated playlist explaining : - (i)rocket science (40 min video ) (ii)how do gov and priv space agencies get their fuel in india

@ashishranjantalks 3 года назад

Will try

@siddhantdogra9947 3 года назад

SpaceX's Rockets first stage boosters are reusable and they are not only designed to launch payload to orbit but in addition they have to return back to the ground which is a really complex task and requires multiple ignitions in combustion chamber which is not fulfilled by solid propulsion engine. Another reason to use liquid propulsion engine is that they need lots of fuel to launch and land the boosters which is not possible by solid boosters as once ignited its almost impossible to stop the combustion and they will end up having no/low fuel for landing. So, in a nutshell liquid engine provides all the requirements needed for a reusable rockets namely low fuel requirements, multiple ignitions in combustion chamber and above that liquid engines come with a facility of controlling the thrust and its direction which is very essential for the landing of boosters. Adding to this, I am a beginner for learning rocket sciences and do enjoy your lectures.

@ashishranjantalks 3 года назад

Nice. Keep it up

@aktscienceandgaming7487 3 года назад

You helped me a lot

@ashishranjantalks 3 года назад

You're welcome😊

@aktscienceandgaming7487 3 года назад

Sir you made me more confident towards my goal of becoming a rocket scientist when I grow up 😀

@shanmukhshan9650 4 года назад

Brother please upload videos on Stage separation mechanisms...

@ashishranjantalks 4 года назад

Sure

@krishnaraval9802 4 года назад

have you ever heard about a warp drive ??? by the way love your videos keep it up.😁

@ashishranjantalks 4 года назад

Not yet!

@krishnaraval9802 4 года назад

@@ashishranjantalks it is an hypothetical engine or space craft which work on principal of warping space itself that's how we can achieve speed more than light by general theory of relativity.

@mohammadaatif8693 4 года назад

Please make vedio on nuclear science and nuclear reactor as well

@ashishranjantalks 4 года назад

Coming up

@lampospaceagency751 3 года назад

What if I attatched spraying system in front of the two ends of the pipes of the oxidiser and fuel in the combation chamber?? Pls give a reply

@whatif5396 3 года назад

That doesn't work I guess according to fluid mechanics

@lampospaceagency751 3 года назад

@@whatif5396 ok thanks, let ashis sir reply

@harshitpandya3276 3 года назад

Very well explained .....only the board was blur....but overall good explanation👍

@ashishranjantalks 3 года назад

Sorry for that and Thanks😊😊

@dagadulavate3543 4 года назад

U are awesome explanator. How you become a scientist in isro plzzz tell me .

@ashishranjantalks 4 года назад

Thank. by working hard for ICRB

@godzilla18181 4 года назад

Bro what is the actual reason for failure of chandrayan 2

@ashishranjantalks 4 года назад

Nobody knows

@ishukumar9721 4 года назад

Excellent work sir

@ashishranjantalks 4 года назад

Many thanks

@dharmendrabiswal4917 4 года назад

You proved that why mechanical branch is called royal branch.i enjoyed it but something is wrong in light, may be it more brighter so the white board can't clearly visible .

@ashishranjantalks 4 года назад

Yeah, I'll fix it

@abhipandya6456 4 года назад

Space X not using solid booster because it has more weight than liquid.. and also it requires large space than liquid fuel. Am I correct Ashish ..??

@rameshpatil3701 4 года назад

We cannot throttle the solid Propalants

@prabhatbharti4881 4 года назад

Yep, we can't throttle the solid rocket motors, as it ends it's ignition when the fuel is completely exhausted moreover they are dangerous and also called as ' Fireworks ' in branch of rocketry, where as space x reuses it's First stage boosters which needs to be throttled in order to land the boosters precisely on a landing site ( drone ship or ground landing ), the technology is so fun to learn and innovative for me it was like he ( Elon Musk ) used whatever the resources are available here and created a masterpiece ;). Yet many great innovations are yet to happen. I hope one day India will also master cryogenics :D

@ashishranjantalks 4 года назад

Good! but NOt really the reason😊

@nitishshrimal 4 года назад

SpaceX engines are Merlin Engines which uses RP1 as propllant. They also perform landing back to the ground or sea plateform thus they need to be throtteled. Throtling capability lies with liquid engines only. Thus Liquid Engines by SpaceX.

@itss__adityaa 4 года назад

Earlier Im A Fan But Now Im An Air Conditioner

@ashishranjantalks 4 года назад

Hehehehe😂😂😂

@binoybanik9954 4 года назад

What kind of material we use at the throat section to resist High amount of heat ?/ Or how we cooling the throat section to resist melting of the material..!!??

@ashishranjantalks 4 года назад

Ablative material, sometimes we use cooling too

@binoybanik9954 4 года назад

@@ashishranjantalks can you explain about all of these!!!

@ankushmishra1757 4 года назад

Wow! Bro I am a beginner learner of rocket science and your video is osm. And I have got a question in my mind that when the pre combustion chamber is gonna rotate the turbine then how it gonna produce pressure with out air in vaccume?

@ashishranjantalks 4 года назад

Oxidiser is taken along with rocket

@rajendrapal6163 4 года назад

Everything, from enthusiasm to the level of knowledge was awesome but board is a quite small and the written part becomes harder to read . Kindly use a big board or a black board because then the visibility would be more clear and the diagram would be bigger enough to understand 👌👌👌.

@ashishranjantalks 4 года назад

Sure, will do when channel becomes bigger

@yogitasharma4619 3 года назад

Not visible properly... But overall a nice explanation👍👍... Can u suggest some Magazines for beginner to know more about rocket science..???

@ashishranjantalks 3 года назад

Noted

@praveenchoudhary9956 4 года назад

I have some queries 1) Why isro can't make a complete new design rocket engine , I mean you know vikas and sce200 both are foreigners design base 2) is isro working on methane fule powered engine 3) can isro make heavy launch vehicle by using sce200 4) what about admire rocket How much time it will take to come in final operation 5) what will be final product of rlv -td I hope you will answer 🙂🙏

@ashishranjantalks 4 года назад

1. ISRO has already made indigenous cryogenic stage used in MkIII 2. That I cannot talk about 3. It's possible 4. That I cannot talk about 5. That I cannot talk about Don't ask me questions related to ISRO, this series is on rocketry in general

@praveenchoudhary9956 4 года назад

@@ashishranjantalks thanks

@mohammedmusaghori9914 4 года назад

Sir, please explain about various tests performed on solid rocket motors ,on different stages of liquid propellant engines and flight control tests on launch vehicles at isro.

@ashishranjantalks 4 года назад

Ok😊👍

@adityabaware5857 2 года назад

Plz post more videos

@shivanshjzr1316 4 года назад

Video dekhne se pehle hee like or comment kr diya kyuki mujhe pta h video achha or knowledgeable hee hoga

@ashishranjantalks 4 года назад

Thanks Shivansh😊😊

@aarvraina1785 2 года назад

Anyone in for making rocket...a differrnt and reusable one.....from India....😚😊

@dhrupadsaha4171 4 года назад

Great Content Sir

@ashishranjantalks 4 года назад

Thanks😊

@scientistanurag7768 4 года назад

Sir I want to be a scientist, please make video on how to take job as a scientist. Please sir✌️✌️🙏

@bishwayan2410 4 года назад

Hey, ASHISH plz make more videos on rocket science, explaining different aspects of it. Because you teach it in an amature way without going super deep. It's great.

@ashishranjantalks 4 года назад

Sure I will

@venka4921 4 года назад

India is not using liquid engines in 1st state is to make the launch vechile more cheap and Sir can u explain y India is not doing spacex thing(reusable ) instead doing like space shuttle (rlv td ) India also should land booster like spacex since it will increase the accuracy of landing which will help in more other missions like chandrayaan 2. what is your opinion sir

@ashishranjantalks 4 года назад

The only reason I can think of is maybe they are planning to make their own ISS

@venka4921 4 года назад

@@ashishranjantalks Sir love your videos I am a student of 10. I am very much interested in rocket science please make a video about semi cryogenic engine . it would be better to have moon base than iss

@Bobby_baghel.b 4 года назад

Thank you sir this series really help full ,💜💜💜💜💜💜♥️♥️♥️♥️♥️

@ashishranjantalks 4 года назад

Most welcome

@aanchaljaiswal1680 4 года назад

Very nice explanation sir. My answer to the question you asked is In liquid engines we can control the combustion and we can start and stop the engine multiple times as per our requirement for example when the satellite needs to be put on the orbit ( told by you only :))

@ashishranjantalks 4 года назад

Yes, correct😊

@aanchaljaiswal1680 4 года назад

Sir at the time of docking also engine needs to be started and stopped multiple times?

@PavanSpace 2 года назад

@@aanchaljaiswal1680 Yes!

@off3425 Год назад

Sir, I'm in class 11 and i want to be a rocket scientist in future. How should I start

@upendravirkar6222 4 года назад

sir my question is , what are the metals or any alloys are use to make these pumps and combustion chamber and shafts , as temperature is very very high like 250 bar or 300 bar .

@ashishranjantalks 4 года назад

They are made of steel and aluminium only

@Topn08_ 3 года назад

I like the way you explaining 😁

@ashishranjantalks 3 года назад

Thank you! 😃

@Topn08_ 3 года назад

@@ashishranjantalks always welcome r you malayali

@Topn08_ 3 года назад

@@ashishranjantalks I am Arun from Kerala.now am making a sugar rocket so I wanted to know about nozzle thats why I came here.any way it was great 😁❤️

@vaibhavmishra1914 3 года назад

superb Dude.

@ashishranjantalks 3 года назад

Thanks a lot 😊

@SandeepReddy-ou4zp 4 года назад

The main difference between solid rocket engine & liquid rocket engine is that we can control fuel rate.thus we can control the combustion process the fuel engine.but it's not possible in solid engine right Ashish!

@ashishranjantalks 4 года назад

True

@smrutiranjansahu678 3 года назад

I wanna be start a aerospace start up.Tell me where can i find skilled people who can help me in future ?? And can i make my own parts ?

@ashishranjantalks 3 года назад

@godgiftedaradhya9558 4 года назад

Sir how propellant provide cooling to the engine

@ashishranjantalks 4 года назад

as it's at much lower temp than hot gas, it is circulated around hot parts of engines before it is fed to combustion chamber

@GaneshmPatil 3 года назад

Very well explained..can some one please explain how spacex rockets come on exact same point after launch

@ashishranjantalks 3 года назад

I'll try to explain soon

@lordfoj9828 4 года назад

16:41 Space x need to land their stages back to earth, they will need a proper toogle control over the stage so they use liquid engine.

@ashishranjantalks 4 года назад

Correct

@shlokjadhav8253 4 года назад

I was also gonna reply the same. Thank you for saving my efforts

@scientistanurag7768 4 года назад

@@shlokjadhav8253 same to you

@aanchaljaiswal1680 4 года назад

Sir, at the time of docking also engine needs to be started and stopped multiple times?

@ashishranjantalks 4 года назад

yes

@scientistanurag7768 4 года назад

Nice question

@shiVam01242 2 года назад

Valuable 😊😊

@ashishranjantalks 2 года назад

Always 🙌

@sirdhartharoy9553 Год назад

Achha viya ap konsa marker use kar rehe he marker ka name bata sekte he pls, i need marker of good quality

@ashishranjantalks Год назад

4 saal purana video hai bhaai

@vaibhavshende2642 4 года назад

Using the same combustion chamber for turbine we can regulate/maintain the rpm of centrifugal pump more easily so that they can pump some what more amount of fuel and oxygen mixture and increase the thrust. Then why we use other combustion chamber ? Which have different pressure generated in it. Using same combustion chamber will be easy n will decrease the weight too which is a main factor.

@ashishranjantalks 4 года назад

It'll be a very complicated design otherwise

@vaibhavshende2642 4 года назад

@@ashishranjantalks Ok sir

@veera7391 4 года назад

Just finished your unacademy Vedio...😍

@ashishranjantalks 4 года назад

Great 👍

@vikashnasharma5724 Год назад

Imagine that you are on a street with houses marked 1 through n. There is a house in between (x) such that the sum of the house numbers to the left of it equals the sum of the house numbers to its right. If n is between 50 and 500, what are n and x?'

@kabin3364 4 года назад

Everyone in the comment section are thinking space x uses liquid engines just because they are stable. They are not stable on themselves only. They are stabelized by active thrust vector control which is due to different sensors like accelerometer, gyroscope, gps, barometric pressure sensors and other subcomputers present in flight computer of the rocket.

@ashishranjantalks 4 года назад

true

@riddhibhattacharjee8440 2 года назад

Sir , can we increase the thrust of the rockets by decreasing the area of cross-section and increasing the lower part of the nozzle ?

@ashishranjantalks 2 года назад

Pressure thrust = Pressure difference * area

@parulsingh9181 3 года назад

I want to make a working model of a rocket for my project and also I want to explain it in very simple word can u pls give me some tips on that.

@ashishranjantalks 3 года назад

Sure What help do you need

@bidyutgogoi8668 4 года назад

Bro please explain about hybrid rocket engine too

@ashishranjantalks 4 года назад

Sure😊

@bidyutgogoi8668 4 года назад

Thnkss ❤️

@Starman5771 4 года назад

Plz do make a video on possible failures in turbopump

@ashishranjantalks 4 года назад

@sonil9878 3 года назад

Spacex does not use solid boosters because solid boosters do not allow for good regulation of thrust(i.e. increasing or decreasing thrust). Another problem with solid boosters is that they are hard to turn off and on again, which is an important requirement for spacex since they are building reusable rocket engines. Am i correct?

@ashishranjantalks 2 года назад

Not really It’s connected to reusibility

@toxik5332 3 года назад

Bhaiya pls make for space X landing also

@ashishranjantalks 3 года назад

Will do

@priyanshgarg7122 4 года назад

Why ISRO's PSLV the most successful rocket of ISRO till now has most of its stage as solid?

@ashishranjantalks 4 года назад

It's robust and tested

@thugmohan6637 3 года назад

Osm bro

@ashishranjantalks 3 года назад

😊😊

@nikhilkolhe2374 2 года назад

because for landing the boosters upright they need to restart the engine. Which as explained by you not possible with solid engines

@sayanchakraborty6379 4 года назад

I have a doubt, can you please tell me "which force comes earlier on an object moving in curved path, centripetal or centrifugal force? "

@ashishranjantalks 4 года назад

They come simultaniously

@sayanchakraborty6379 4 года назад

@@ashishranjantalks thank u

@aftab2360 4 года назад

After separation they want to bring back the rocket boosters, to do so they need controllable combustion that’s why they use liquid motor engine in boosters which fullfill the desired needs instead of solid rocket motor engines ,because they can’t...

@ashishranjantalks 4 года назад

True

@pavankalyan6702 4 года назад

Very nice explanation sir easily understandable..😍keep more videos on rocket science I have much interest on it.I want to learn more about this....

@ashishranjantalks 4 года назад

Sure I will

@souravkumar2909 3 года назад

What is difference btwn cryogenic engine and scramjet engine.which is more advance.plz make a video

@ashishranjantalks 3 года назад

Scramjet is air-breathing

@ranusoni1178 4 года назад

Plz.. tell us about the role of automation in mechanical engineering..

@ashishranjantalks 4 года назад

Robotics

@souravkumar2909 3 года назад

Sir request u to make board visible as light intensity is Vry high making unable to see it.plz look into matter

@ashishranjantalks 3 года назад

Sure, working on it

@kushmandey6880 4 года назад

How do you design the combustion chamber so as to maintain high pressure

@ashishranjantalks 4 года назад

Pressure vessel design knowledge is needed

@kushmandey6880 4 года назад

@@ashishranjantalks Could you provide a references like books or topic I can study in detail

@abhipandya6456 4 года назад

Thank you Ashish... Can you just tell me the fuel and oxidiser name that ISRO use frequently..

@ashishranjantalks 4 года назад

UDMH, n2O4 LOX, LH2

@sriramswain3864 4 года назад

Will there be any video for Guidance Navigation and Control sir

@ashishranjantalks 4 года назад

Yes

@somprabhatsharma3952 4 года назад

Hi sir can you please suggest me some good books for cfd . Or any free online content to learn cfd (computational fluid dynamics) or tell me the way how I should learn cfd . I have been following you for last nine months . Your content is awesome sir plss help me if possible

@ashishranjantalks 4 года назад

Follow NPTEL lectures but S chakrawarti These are videos that I made Water Jacket Project: ru-vid.com/video/%D0%B2%D0%B8%D0%B4%D0%B5%D0%BE-uhXF-ZT47JM.html Insulation thickness Project: ru-vid.com/video/%D0%B2%D0%B8%D0%B4%D0%B5%D0%BE-Sy42-59YmmY.html

@somprabhatsharma3952 4 года назад

@@ashishranjantalks thank you so much sir Is nptel lecture enough to learn cfd

@sonil9878 3 года назад

Sir in this video you talk about closed loop system. I have heard about open loop systems as well, plz do make a video about them as well. And awesome job in explaining it in layman's terms

@ashishranjantalks 2 года назад

Will do It’s actually an open loop only But easier to understand link this

@AeroSpaced296 4 года назад

Buddy ! I just saw a video from ARCA space a private rocket company trying to make SSTO rockets which is powered by water can you please analyse it and make a video on it. I would like to know more about flight computers used on rockets and what type of chip does isro use . And please make a video on orbital mechanics too sorry my list might be big.

@ashishranjantalks 4 года назад

I'll try but I think Scott Manly did a very good breakdown

@shubhamsinha1330 3 года назад

the light was falling on the board so it was a bit difficult to read i hope you can fix it

@ashishranjantalks 3 года назад

Yes, will fix it in future