Recent content by MechanicalMan

  1. M

    MATLAB Create Table for Matlab Newtonian Cooling Solution

    Hi all, I'm writing a program for a graduate level course that I'm taking wherein I'm solving the Newtonian cooling solution for a long metal rod with specified properties. I have no problem setting up the code and generating a plot, but I am running into problems creating a table of the...
  2. M

    Advanced Heat Transfer - Conduction Cooling in Turbine Blade

    I managed to solve the problem, and after pages and pages of algebra, I have the solution in terms of hyperbolic functions. Thanks for the tips.
  3. M

    Advanced Heat Transfer - Conduction Cooling in Turbine Blade

    Thanks, I did make some typos in the original statement, which is why it may seem off at some points. I did miss the negative root and I did miss the x in the exponent of my original post. I have the boundary conditions, but my only concern is that if I relate the heat transfer by convection at...
  4. M

    Advanced Heat Transfer - Conduction Cooling in Turbine Blade

    I am trying to solve an advanced heat transfer problem and I have a 2nd order ODE. I can solve the homogeneous solution easily, but I am having trouble with the non-homogeneous solution.Homework Statement Given a turbine blade and asked to model as a one-dimensional fin, subject to the...
  5. M

    If angle lies in second Quadrant?

    The vertical axis (y-axis) is considered to be x = 0 (in the cartesian plane). Therefore, any point (x,y) in the second quadrant will have a negative x value and a positive y value. Consult this link here if you require more information: http://en.wikipedia.org/wiki/Cartesian_coordinate_system
  6. M

    Exploring Level Surfaces of a Multivariable Function

    What is the problem statement? You can't be just given an equation and asked to solve it. Your question is too ambiguous.
  7. M

    What Values of (x, y) Make f(x, y) = 1/(x - y^2) Undefined?

    Ask yourself this question, and you'll have answered your own question: For what values of (x,y) is f(x,y) undefined?
  8. M

    What Is the Minimum Diameter of a Duct to Limit Head Loss to 20 Meters?

    My piping systems design textbook says that for a smooth pipe, you can take your roughness e = 0.0015mm. Try that and see what kind of answer you come up with.
  9. M

    What Is the Minimum Diameter of a Duct to Limit Head Loss to 20 Meters?

    Seeing how you don't have velocity or friction factor leads me to believe that this might be an iterative solution. Assume a value of velocity, use that to find your Reynolds, find your friction using the Colebrook equation. Find the diameter. Rinse and repeat until you get some sort of...
  10. M

    Civil Engineering - Do All Engineers Study the Same?

    It's funny that you ask that question, about whether Civil engineering is easier than other fields. I have a few friends who are in Civil (or "simple" engineering, as we call it) who often complain about the workload. A lot of their courses (from what I hear) are pretty much the same thing...
  11. M

    What Is the Minimum Diameter of a Duct to Limit Head Loss to 20 Meters?

    Do what you were doing in the first attempt, with V = Q/A. Keep in mind that A = (pi/4)*D^2
  12. M

    Heat Transfer: Calculating Time to Heat 1000L of Water

    Well, whenever I'm trying to find how long it would take some to heat up or cool down, I always think of Lumped Systems Analysis, as there is a time rate term in the equations. Essentially, the energy balance breaks down into {Change in Internal Energy During Time Interval dt} = {rate of heat...
  13. M

    Mechanics Question on Vibrations

    Try using Lagrange's equations to solve for the equations of motion. It's a lot simpler to find the equations of motion with Lagrange's equations (providing you don't leave out any of the terms). After you find them using Lagrange's equations, you can put it into a matrix, find the...
  14. M

    Heat Transfer: Calculating Time to Heat 1000L of Water

    Have you studied Lumped Systems Analysis?
  15. M

    Understanding Lift Generation and Investigating Results

    Essentially, lift is due to circulation. Circulation will occur in flow over an airfoil because of flow separation, which occurs due to a stagnation point near the back end of the airfoil. Try playing around with this website: http://www.grc.nasa.gov/WWW/K-12/airplane/foilsimu.html. You can...
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