Throat temperature & exit velocity of rocket engine nozzle | GATE AE 132 | Propulsion - YouTube
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![Axisymmetric simulation of a rocket Mortar exhaust in Ansys Fluent [Dissertation Project] By Rokas Simonis, Supervisor: Dr Bidur Khanal | Rokas Simonis Engineering Portfolio](http://simonis.coventry.domains/wp-content/uploads/2019/05/Capture53-1.png "Axisymmetric simulation of a rocket Mortar exhaust in Ansys Fluent [Dissertation Project] By Rokas Simonis, Supervisor: Dr Bidur Khanal | Rokas Simonis Engineering Portfolio")
Axisymmetric simulation of a rocket Mortar exhaust in Ansys Fluent [Dissertation Project] By Rokas Simonis, Supervisor: Dr Bidur Khanal | Rokas Simonis Engineering Portfolio
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Nozzles
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