Mod-01 Lec-10 Nozzles Shapes

[@ravi99217]

note 33:40 combustion instability, at throat acts like closed end not open end

[@abhijithmr9609]

extremely understandable..great teaching sir

[@muddalthirumalesh3199]

Thank you sir ,but i have doubt that Why did u calculated change in moment for the sound in a pipe, and why did u replace the change in density in the nozzle equation to change in density of sound in a pipe,plz clarify the doubt sir

[@joliverkozlowski]

up

[@shivangsingh5834]

There's nothing very big logic here we want a design parameters depending upon we can design a nozzle or diffuser for our Rocktes Bernoulli equation helps in understanding how area and velocity are related but it has limitations using Bernoulli you can't design nozzle for let's say supersonic nozzles or hypersonic nozzle there you need different kind of physics this we are just correlating how area's and velocity related in compressible flow and high-speed aerodynamic that's it I hope you understand

[@daujok1301]

Thank you professor! This is an exciting stuff!!

[@fromthenorthfromthenorth8224]

Thank you professor! from Canada

[@claire8121995]

Please change the subtitles from mock to mark I presume ... let me know if it is really mock or mark

[@scp_at_iitb]

It is Mach actually

[@VijayaOrganics]

Thank you very much Sir.

[@sanjayganesh6760]

Thank you

[@chandrashekhar-oq8io]

Thanks a lot 'my lord'. For making me understand..

[@rauffux]

thank you from portugal!

[@w98BnqA3]

Thanks Prof!

[@debarshibiswas3285]

thank you sir

[@jaybabcock9123]

If only i understood half of the basic physics principals needed ☹️

[@BLAC3546]

thanks pro.

[@yashpatole3108]

thanks sir

[@daujok1301]

Thank you professor! This is an exciting stuff!!