1- The concentric wave circles in stationary point source in a con 2- The changing in static pressure with x-axis of gas expanding fi divergent nozzle ( curve B & C) 3- The exit properties of air flowing in constant area duct with su process.

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Analyze :
1- The concentric wave circles in stationary point source in a compressible fluid
2- The changing in static pressure with x-axis of gas expanding from tank to convergent-
divergent nozzle ( curve B & C)
3- The exit properties of air flowing in constant area duct with subsonic flow and heating
process.
Transcribed Image Text:Analyze : 1- The concentric wave circles in stationary point source in a compressible fluid 2- The changing in static pressure with x-axis of gas expanding from tank to convergent- divergent nozzle ( curve B & C) 3- The exit properties of air flowing in constant area duct with subsonic flow and heating process.
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