TIME STAMPS 05:55 STEAM NOZZLE STARTS 14:30 TYPES OF NOZZLES 33:30 FLOW IN A NOZZLE 40:30 CALCULATION OF EXIT VELOCITY IN NOZZLE 49:10 DISCHARGE THROUGH ISENTROPIC NOZZLE 53:50 CONDITION FOR MAX DISCHARGE 01:00:20 CRITICAL PRESSURE RATIO 01:12:00 SIGNIFICANCE OF CRITICAL PRESSURE RATIO
The way of delivering concepts are extraordinary amazing. My field is Electronics and i am doing MS in Power Engineering i.e didn't have basic knowledge of mechanical but this lecture clears my all concepts about Steam Flow Nozzles. Thanks alot love from Pakistan!
According to Zenner equation n for wet steam is, n= 1.035+0.1x where x is dryness fraction. So sir how did you calculated critical pressure ratio of wet 💦 steam as it depends upon dryness fraction.
sir what is the ratio of length between coverging and diverging section.?diverging section is quite larger in length than converging but how many times?
m2 = -1 aap nhi daal sakte kyoki yeh not define h aur m = -1 ka koi matlab nhi h mach no. speed of body to speed of sound ka ratio h vo negative kese hoga aur agar v1 dale toh zero ho jayga uska matlab area not change jo hota h throat par uniform cross section hota h 👍👍👍
Sir at 1:14:06 what you are teaching is wrong because at that pressure is sam everywhere so there will be no flow initially ...but according to you if exit pressure is more the flow will be backward. So correct there
TIME STAMPS
05:55 STEAM NOZZLE STARTS
14:30 TYPES OF NOZZLES
33:30 FLOW IN A NOZZLE
40:30 CALCULATION OF EXIT VELOCITY IN NOZZLE
49:10 DISCHARGE THROUGH ISENTROPIC NOZZLE
53:50 CONDITION FOR MAX DISCHARGE
01:00:20 CRITICAL PRESSURE RATIO
01:12:00 SIGNIFICANCE OF CRITICAL PRESSURE RATIO
Rahul sir us backbone of mechanical engineer thanks a lot sir !!! Great Lecture Great teacher
লাইক
सर आप का कोई जवाब नहीं है।इतना अच्छे से समझाते है।आपका का क्लास देखकर ऐसा लगता है कि पीछे कुछ पड़े ही ना हो।
general engineering ka preparation isi lecture se kr rhe sir...maza aa gya padh kr ..lazawaab
Sir ,Ek Lecture Hot Air preheating per bhi rakhe ,Aap ekdam excellent Lecture dete ho .Good job by u .God bless u.🎉🎉🎉🎉🎉🎉🎉
@RpDilkochoonewalasongSidhu thank you dear
The way of delivering concepts are extraordinary amazing. My field is Electronics and i am doing MS in Power Engineering i.e didn't have basic knowledge of mechanical but this lecture clears my all concepts about Steam Flow Nozzles. Thanks alot love from Pakistan!
bahut sandar jabbardast lecture sir,,,,, is bar sb ka beda par,,,,,, thank u sir ,,,,,,
You are really an amazing teacher.
its very simple way of learning. Really its MAKE IT EASY.
Rahul sir is a brand for Mechanical engineering
sir every time i learn something new from yr video thank so much
Very helpful lecture sir. Thanks a lot for your effort.
Thnks a lot this topics is core and it will come definitely in ssc JE 🙏
Thanks a lot sir, keep making videos... Very helpful for non-mechanical people also...
Thank you sir...
Thank you for tricks.
Thanks sir...💐👍💐👍 !!!!!!
hidden gems for AE/JE Student.
First time read and understand
TQ sir apko ❤️❤️❤️
Awesome lecture sir thanxx for ur effort everyday increase my confidence...
Best Exiplenation sir
Sir my present state is like ur past.. I feel more confident in history than technical
Could i subscribe multiple times but like millions time👍👍👍👍👍👍👍👍👍
aaj pehli baar pta laga ki aapne history b pdai h
Class starts at 06:00
Good morning sir 🙏🙏🙏
Sir I am from Indian navy and i am watching this video
I am very satisfied
Very good explained
Thank you sir for all ur efforts. 🙏🙏
Excellent sir....
I appreciate you.
According to Zenner equation n for wet steam is, n= 1.035+0.1x
where x is dryness fraction.
So sir how did you calculated critical pressure ratio of wet 💦 steam as it depends upon dryness fraction.
Dhasu lecture sir...👌👌👌👌
THANKS A LOT❤
Overall I appreciate your way of teaching 😊 Sir
great lecture sir. thank u
Very nice sirr
Thank you sir bhut achaa lecture tha
sir what is the ratio of length between coverging and diverging section.?diverging section is quite larger in length than converging but how many times?
Tq for Valuable effort sir... I think efficiency of nozzle is not included please include that in Short video 😍
Sir ham polytechnic kar rahe h , hame full detail or derivated concept chaiyega , toh hamare liye ye sahi h kya
Lagabab lecturer for me
Thank you❤❤❤
Amazing explation sir
Sir but mach no and mech nonis different na?
For flow through nozzle and diffusers,which fluid property remains constant ?
a) enthalpy b) velocity c) stagnation enthalpy d) entropy.
Entropy
Thanks a lot sir
Nice session thank you sir
Sir equation me agar M² me -1 put karenge to 1 aayegana , then it will look like dA/A=dV/V(1-1), fir 0 aayegana sir ,ye case samjayeye plz
m2 = -1 aap nhi daal sakte kyoki yeh not define h aur m = -1 ka koi matlab nhi h mach no. speed of body to speed of sound ka ratio h vo negative kese hoga aur agar v1 dale toh zero ho jayga uska matlab area not change jo hota h throat par uniform cross section hota h 👍👍👍
Adorable
i'm a new subscriber
good
Sir at 1:14:06 what you are teaching is wrong because at that pressure is sam everywhere so there will be no flow initially ...but according to you if exit pressure is more the flow will be backward. So correct there
Thanku so much sir
Sir aap book ka name bta skte h?
Nice class sir
thanku sir
Thanks sir
sir practicle example hai rockets ke outer nozzle diverging hote hai today i understand why
Sir apne confusion ko permanently zero kar diye hai sir
CASTING AND FORGING SIR
Sir p2 exit conditon ka nahi h .p2 thorat ka pressure hain
Video not running properly
Lecture is modifing add h kuch concept
Sir may mechanical ka student hu sir THERMAL ka may pura vidao kha se dekhe jo pura mil jaye sir plzzz
👌👌
No
Bakwas
Rip
Thank you sir
Thanks sir
Thanks sir ❤️🙏
Thanks sir