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Which formula do we have to use to calculate the difference between the inlet and throat , correctly? is it the one whereby we divide (Q/Cd×A)² by 2g or the one with 2gh/2g
Hi the first one is best
Is it possible to obtain a negative h?
h must be positive always since it's bigger height- the smaller one
Which formula do we have to use to calculate the difference between the inlet and throat , correctly? is it the one whereby we divide (Q/Cd×A)² by 2g or the one with 2gh/2g
Hi the first one is best
Is it possible to obtain a negative h?
h must be positive always since it's bigger height- the smaller one