Converging-Diverging Nozzle - Lesson 4

This video lesson describes converging-diverging nozzles, which have an hourglass shape with a minimal area in the throat region. These nozzles are used to accelerate flows to very high speeds in aircraft and spacecraft. This lesson is part of the Ansys Innovation Course: Internal Compressible Flows. To access this and all of our free, online courses - featuring additional videos, quizzes and handouts - visit Ansys Innovation Courses at www.ansys.com/....

[@yashgolwala5290]

Best video on this topic!

[@mdabdullahalmamun5067]

Organized Explanation. Thanks

[@ahmetkirhan5896]

Thanks for the video!

[@AnsysLearning]

Thanks for watching! Visit Ansys Innovation Courses for free courses, including videos, handouts, simulation examples with starting files, homework problems, and quizzes here: ansys.com/courses.

[@michaelgarcia812]

Nice job!!

[@AnsysLearning]

Glad you liked it! Visit Ansys Innovation Courses for free courses, including videos, handouts, simulation examples with starting files, homework problems, and quizzes here: ansys.com/courses.

[@Indonesia01ian]

Hi everyone, I am sorry, I still don't get the point what really happens if incompressible fluid flow through the CD nozzle? why the density change can affect the acceleration of the compressible fluid
thanks

[@concertoquarantasei4143]

can i have all the picture

[@kenneth_mirez]

the bakcground music was distracting

[@AnsysLearning]

Thanks for watching & providing feedback! Visit Ansys Innovation Courses for free courses, including videos, handouts, simulation examples with starting files, homework problems, and quizzes here: ansys.com/courses.

[@muhammadtalhaarif2249]

Why you are laughing while telling sir??😂

[@AnsysLearning]

Thanks for watching! Please post your query on the Ansys Learning Forum for a detailed answer from the wider Ansys Community: ansys.com/forum.