1. Limited time only! Sign up for a free 30min personal tutor trial with Chegg Tutors
    Dismiss Notice
Dismiss Notice
Join Physics Forums Today!
The friendliest, high quality science and math community on the planet! Everyone who loves science is here!

Heat Transfer - Viscosity questions

  1. Oct 4, 2016 #1
    1. The problem statement, all variables and given/known data
    I do not need to solve this problem, see below.
    EXAMPLE 7.1
    Air at a pressure of 6kN/m2 and a temperature of 300C flows with a velocity of 10m/s over a flat plate 0.5m long. Estimate the cooling rate per unit width of the plate needed to maintain it at a surface temperature of 27C.

    2. Relevant equations
    Kinematic viscosity

    3. The attempt at a solution
    My question is about the very first/second step, I have attached pictures showing the example problem and the table A4 from the back of the book.
    1. How did they decide on the temperature 437K to use in the table.
    2. And why is the viscosity 10^-6? Not 10^6?
    3. I see that the description mentions something about the inverse viscosity, can anyone elaborate a little about that?
    4.Last question is on the 3rd image it shows the Reynolds number is ~9000, isn't that a turbulent flow, but they say its laminar? According to wikipedia laminar flow is less than 2000 correct?

    Thanks for any help, I just want to understand the concepts going on. No need to solve the problem.

    Attached Files:

    • 1.JPG
      File size:
      8.5 KB
    • 2.JPG
      File size:
      23.4 KB
    • 3.JPG
      File size:
      15.8 KB
    • 4.JPG
      File size:
      23.5 KB
  2. jcsd
  3. Oct 4, 2016 #2
    I have no idea. Maybe they meant 200 C in the problem statement insteady of 200 C, in which case the temperature would be 473K.
    Look at the heading at the top of the column. It says ##10^6\nu##. That means that each of the numbers in the table has been obtained by multiplying the actual ##\nu## value by ##10^6##
    It says that the kinematic viscosity of a gas is inversely proportional to the pressure. Do you know what this means mathematically? What pressure do the values in the table apply to?
    The laminar-turbulent transition depends on the specific geometry. The value of 2000 corresponds to flow in a tube. The critical Re for flow over a flat plate is much larger. Why don't you research it an get back with us?
  4. Oct 4, 2016 #3
    Thanks for the help!

    Well viscosity increases with an increase in pressure. Based on the equation for kinematic viscosity, kviscosity=viscosity/density, if viscosity and pressure are both increasing, shouldn't the kinematic viscosity be increasing as well?

    OK got it, pretty simple. Re for turbulent flow over a flat plate is 10^8.
  5. Oct 4, 2016 #4
    For an ideal gas (and for real gases at low pressures), viscosity is independent of pressure (see Transport Phenomena, Bird, Stewart, and Lightfoot, Chapter 1) and density is proportional to pressure. So kinematic viscosity is inversely proportional to pressure.
Know someone interested in this topic? Share this thread via Reddit, Google+, Twitter, or Facebook

Have something to add?
Draft saved Draft deleted

Similar Discussions: Heat Transfer - Viscosity questions
  1. Heat Transfer Question (Replies: 0)