Find the field flow using integrals

In summary, the conversation discusses finding the flow of a field F through a given surface S. The equation of the surface is given as 4x+2y+z=6, and the coordinates x, y, and z must be non-negative. The solution involves evaluating a surface integral, and the divergence theorem can also be applied. There is also a discussion about the orientation of the surface and the use of a unit normal vector in the calculation.
  • #1
kliker
104
0

Homework Statement


find the field's F flow where F = (y,-z,2) through the surface S where S is 4x+2y+z=6 and x,y,z>=0

The Attempt at a Solution



we know that

[PLAIN]http://img195.imageshack.us/img195/4971/asdqg.gif

we know F

N is the derivative of 4x+2y+z-6 = g(x)

actually it's N = (dg/dx,dg/dy,dg/dz)

now what i want to ask is how to find the limits of the integral i mean from what point to what point i should integrate

what I can think of is because x,y,z are bigger than 0 hence they are possitive

we will have the same points for dy and dx which will be from 0 to +oo

so can i just say

[PLAIN]http://img514.imageshack.us/img514/351/asdd.gif

find the integral and then take the limit using xn -> oo and yn -> oo?

thanks in advance

edit: but i have a z, what am i going to do with z?
 
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  • #2
You need to evaluate a surface integral. Rewrite the equation of the plane in the form z = f(x, y), plug it into your integral, and find the triangular region over which you need to integrate, together with the appropriate boundaries of integration.
 
  • #3
By the way, applying the divergence theorem yields the answer very quickly.
 
  • #4
4x+ 2y+ z= 6 is a plane. Since "x, y, z>= 0", that is, all coordinates must be non-negative, you want the portion of the plane that is in the first octant. It's boundary consists of points where some of x, y, z are equal to 0. Specifically in the xy-plane, where z= 0, the triangular region radou referred to has boundaries x= 0, y= 0, and 4x+ 2y= 6 so that y= 2x- 3. y will also be 0 when 2x- 3=0 or x= 3/2.

x goes from 0 to 3/2 and, for every x, y goes from 0 to 2x- 3.
 
  • #5
thanks for your help guys

one last question

should I replace z = 6-2y-4x if i have a z in the integral?
 
  • #6
radou said:
By the way, applying the divergence theorem yields the answer very quickly.

No, it doesn't. You don't have an enclosed volume.

kliker said:
thanks for your help guys

one last question

should I replace z = 6-2y-4x if i have a z in the integral?

Yes. But I have a couple of questions for you. First, did you check the orientation of the surface and do you know you are calculating the flow in the proper direction?

Second, you apparently got your normal vector by taking the gradient of the plane equation, which gives the coefficients. But [flux] surface integrals are of the form

[tex]\int\int_R \vec F \cdot \hat n\ dS[/tex]

using a unit normal, which your N isn't. Now it turns out that your integrand is correct but my question to you is do you know why or did you just get lucky? Why did you not use the unit normal? Are you using something you didn't tell us?
 
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  • #7
radou said:
By the way, applying the divergence theorem yields the answer very quickly.

LCKurtz said:
No, it doesn't. You don't have an enclosed volume.
But Stoke's theorem could convert it into an integration around the bounding triangle. That probably would be harder, not simpler!
 
  • #8
LCKurtz said:
No, it doesn't. You don't have an enclosed volume.
Yes. But I have a couple of questions for you. First, did you check the orientation of the surface and do you know you are calculating the flow in the proper direction?

Second, you apparently got your normal vector by taking the gradient of the plane equation, which gives the coefficients. But [flux] surface integrals are of the form

[tex]\int\int_R \vec F \cdot \hat n\ dS[/tex]

using a unit normal, which your N isn't. Now it turns out that your integrand is correct but my question to you is do you know why or did you just get lucky? Why did you not use the unit normal? Are you using something you didn't tell us?

We ve learned in Math that field flow has this kind of integral, that's why I used it

the reason i used simple F and N is because i don't know how to create a vector F and N on my keyboard
 
  • #9
LCKurtz said:
Yes. But I have a couple of questions for you. First, did you check the orientation of the surface and do you know you are calculating the flow in the proper direction?

Second, you apparently got your normal vector by taking the gradient of the plane equation, which gives the coefficients. But [flux] surface integrals are of the form

[tex]\int\int_R \vec F \cdot \hat n\ dS[/tex]

using a unit normal, which your N isn't. Now it turns out that your integrand is correct but my question to you is do you know why or did you just get lucky? Why did you not use the unit normal? Are you using something you didn't tell us?

kliker said:
We ve learned in Math that field flow has this kind of integral, that's why I used it

the reason i used simple F and N is because i don't know how to create a vector F and N on my keyboard

I wasn't asking because of the typing. I was asking because you didn't use a unit vector in your calculation. Your N is not a unit vector. And dS is not dxdy. I was wondering if you could explain about that. And you didn't answer the question about the orientation of the surface. Which way is it oriented and does your choice of normal agree with it?
 

FAQ: Find the field flow using integrals

1. What is the concept of finding the field flow using integrals?

The concept of finding the field flow using integrals involves using mathematical integration to calculate the total flow of a vector field over a given surface or region. This allows us to determine the magnitude and direction of the flow at any point in the field.

2. How do you set up the integral to find the field flow?

To set up the integral, we first need to define the vector field and determine the surface or region over which we want to find the flow. Then, we use the appropriate formula for integrating vector fields, such as the surface integral or line integral, depending on the dimensionality of the vector field and surface.

3. What are some real-world applications of finding the field flow using integrals?

The concept of finding the field flow using integrals has many applications in physics and engineering. It can be used to calculate fluid flow in pipes, airflow around objects, and even the electromagnetic field around a charged particle. It is also useful in analyzing the flow of heat and energy in various systems.

4. Can you explain the difference between a conservative and non-conservative vector field?

A conservative vector field is one in which the total flow around a closed loop is zero, meaning the starting and ending points are the same. This indicates that the field has a potential function and the work done by the field is path-independent. Non-conservative vector fields do not have a potential function and the work done by the field is path-dependent.

5. Are there any limitations to using integrals to find the field flow?

While integrals are a powerful tool for finding the field flow, there are some limitations. In some cases, it may be difficult to determine the appropriate surface or region to integrate over, and in more complex vector fields, the integration may be computationally challenging. Additionally, the accuracy of the results may be affected by the precision of the measurements and the assumptions made in setting up the integral.

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