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Rayleigh Flow and Stagnation Conditions

  1. Mar 18, 2015 #1
    1. The problem statement, all variables and given/known data\

    The question I want to ask is how do you relate conditions such as To* and To,1 and To,2, where To,1 and To,2 are the stagnation conditions at the entrance and exit.

    This is the problem I was doing.

    Standard atmospheric air is drawn steadily through an isentropic converging nozzle into a frictionless diabatic (q = 500 kJ/kg) constant aread duct. For max flow, determine the values of static temperature, static pressure, stagnation temperature, stagnation pressure, and flow velocity at the inlet [section(1)] and exit [section(2)] of the constant area duct.

    2. Relevant equations


    3. The attempt at a solution
    I know that for maximum flow, To,2 = To*, but I'm not sure if it's due to the fact it's coming in supersonically and because of the heating involved or am I completely off. I also ran into a problem where To,1 = To*
     
  2. jcsd
  3. Mar 24, 2015 #2
    Thanks for the post! This is an automated courtesy bump. Sorry you aren't generating responses at the moment. Do you have any further information, come to any new conclusions or is it possible to reword the post?
     
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