- #1
JuanR43
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Homework Statement
\[/B]The question I want to ask is how do you relate conditions such as To* and To,1 and To,2, where To,1 and To,2 are the stagnation conditions at the entrance and exit.
This is the problem I was doing.
Standard atmospheric air is drawn steadily through an isentropic converging nozzle into a frictionless diabatic (q = 500 kJ/kg) constant aread duct. For max flow, determine the values of static temperature, static pressure, stagnation temperature, stagnation pressure, and flow velocity at the inlet [section(1)] and exit [section(2)] of the constant area duct.
Homework Equations
The Attempt at a Solution
I know that for maximum flow, To,2 = To*, but I'm not sure if it's due to the fact it's coming in supersonically and because of the heating involved or am I completely off. I also ran into a problem where To,1 = To*