hello. video is great , but I have one question. at 5:45, you are saying that as gases goes through divergent passage its velocity is progressively increasing. Shouldn;t velocity decrease and static pressure increase, while gases are going through divergent passage?
Wow. Such a great and excellent. I understood the exhaust so quickly. Thank you for your videos!!!!!!!!!!!
Very nice sir,,, thank you for you presentation about the exhaus GTE
Very very intrested to study
What is the orientation of the Outlet Guide Vanes or nozzle fairings in respect to the turbine blades ?
converging, velocity needs to be increased
hello. video is great , but I have one question. at 5:45, you are saying that as gases goes through divergent passage its velocity is progressively increasing. Shouldn;t velocity decrease and static pressure increase, while gases are going through divergent passage?
Not for sonic & supersonic flow. On converging & diverging nozzles, a supersonic flow experiences the opposite effect that a subsonic flow does.