Physics, 26.06.2019 19:30 elainestorm9633
Discuss where (which component) could be choked condition in a gas turbine ngine, and verify your answer with the geometry of the thrust nozzle design. 1)-for a fighter engine j-79 engine with pressure ratio. 2)-for an advanced commercial engine with pressure ratio
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Discuss where (which component) could be choked condition in a gas turbine ngine, and verify your an...
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