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Search: Posts Made By: arijith
Forum: Main CFD Forum September 28, 2012, 11:18
Replies: 5
Views: 1,396
Posted By arijith
According to the Euler's one dimensional...

According to the Euler's one dimensional compressible equation ..... Mach number has to be 1 exactly at the throat of the nozzle for subsonic flow to become supersonic...if it perturbs a little then...
Forum: Main CFD Forum September 28, 2012, 11:16
Replies: 5
Views: 1,396
Posted By arijith
next one is the question

next one is the question
Forum: Main CFD Forum September 28, 2012, 06:58
Replies: 5
Views: 1,396
Posted By arijith
De Naval Nozzle

Is it possible practiaclly to accelerate a flow from sonic to supersonic flow using Convergent divergent nozzel or De Naval Nozzle ? or is it just an idea? because in every experiment there will be...
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