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Consider subsonic flow at the entrance to a constant area duct which is connected to a diverging nozzle (I.e., at the downstream end of the
Consider subsonic flow at the entrance to a constant area duct which is connected to a diverging nozzle (I.e., at the downstream end of the duct). Can supersonic flow in the nozzle be achieved by adding heating, cooling, and/or friction within the constant area duct? Explain
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