Pressure Nozzle
Good morning (sorry for my english)
but I've this graph
It represent thrust coefficient vs epsilon (ratio area) parameterized by dead end pressure.
The green line is the perfect adaptation. I've these 4 points and I've to create a graph that will show how the pressure goes with the exit area regarding these 4 point.
This should be the solution.
I don't understand point three and four. Can anyone help me??
If it looks like homework, it smells like homework and walks like homework, it is probably time to read our Terms Of Service.
Time to hit the books as I have never seen a homework assignment asking stuff that has not been fully covered in the course notes and lectures.
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