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Question
Helium expands in a nozzle from , and negligible velocity to . Find the throat and exit areas for a mass flow rate of , assuming the nozzle is isentropic. Why must this nozzle be convergingdiverging?
Solution
VerifiedAnswered 1 year ago
Answered 1 year ago
Step 1
1 of 7The stagnation temperature of helium at inlet is:
where is static temperature at inlet, is helium velocity at inlet and is constant-pressure heat capacity of the helium.
If the velocity at inlet is negligible (), then we get:
The stagnation pressure at inlet is given by:
With , and , it is obtained:
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