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Pressure Changes Along Flow Experiencing Heat Transfer

  1. Jun 17, 2016 #1
    For an airflow experiencing a large heat transfer, say a delta of ~600 degrees celsius, I assume compressible effects cannot be ignored. I am struggling however with some conceptual elements, such as how the pressure gradient changes along the flow when compared with compressible and inviscid flow. Is there a technique for calculating both the change in flow rate and temperature at the exit given the rate of heat transfer and entry conditions of the flow?
  2. jcsd
  3. Jun 20, 2016 #2

    jack action

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