Surface Integral, flux. Boundary and orientation

Click For Summary

Discussion Overview

The discussion revolves around the calculation of flux integrals over surfaces, particularly focusing on the influence of the surface's boundary and orientation on the flux. Participants explore concepts related to normal vectors, their magnitudes, and the implications for integrating vector fields across surfaces, including flat and curved surfaces.

Discussion Character

  • Technical explanation
  • Conceptual clarification
  • Debate/contested

Main Points Raised

  • One participant questions whether the boundary of a surface affects the flux solely through integral limits, suggesting that the normal vector does not play a role in this context.
  • Another participant seeks clarification on whether the magnitude of the normal vector is relevant, proposing that only its direction matters for the flux calculation.
  • A different participant agrees with the notion that the normal vector should be a unit normal, indicating that the magnitude is accounted for in the flux component itself.
  • There is a discussion about projecting the surface onto the xy-plane to analyze how different vector field components interact with the surface.
  • One participant emphasizes that on a plane, the normal vector remains constant, while on a curved surface, it varies at different points.
  • Another participant presents a perspective on defining the vector differential of surface area, suggesting an alternative approach to calculating flux integrals that does not rely on unit normals.

Areas of Agreement / Disagreement

Participants express varying views on the role of the normal vector's magnitude and direction, indicating that there is no consensus on how these factors influence the flux integral calculations. The discussion remains unresolved regarding the best approach to defining and using normal vectors in this context.

Contextual Notes

Participants mention different definitions and approaches to normal vectors and surface area differentials, highlighting potential limitations in their assumptions and the need for clarity in definitions.

Liferider
Messages
41
Reaction score
0
In solving a flux integral over a flat surface, inclined above the xy-plane, does the boundary of the surface influence the flux only through the integral limits? (and not through its normal vector)

Let's say that there is an elliptic surface inclined above the xy-plane. The orientation is given by the plane: z=3-y. Now, when I am supposed to solve this surface integral, it seems I can easily use the normal vector of the plane z=3-y in the dS conversion:

dS = [-(∂f/∂x)[itex]^{2}[/itex], -(∂f/∂y)[itex]^{2}[/itex], 1]dA, where f(x,y)=3-y

This means that I do not need to think about the parametrization of the elliptic surface...
This would ofcourse only be true for flat surfaces. So, for clarification, am I doing something wrong?
 
Physics news on Phys.org
To clarify, because this might seem like a strange question... Does the magnitude of the Normal vector play a role, or just its direction?
 
Liferider said:
To clarify, because this might seem like a strange question... Does the magnitude of the Normal vector play a role, or just its direction?

As a disclaimer you should probably get some further input since I haven't taken vector calculus in a long time, but as far as I understand it, the normal vector should be a unit normal and the magnitude should be contained in the information for the actual flux component itself.

If the magnitude was not unit (i.e. 1) then you would have to just normalize the integral in the appropriate way. You have to remember that you are calculating a projection of the flux with respect to the surface normal and if you review the definition of such a projection, you should find that the normal needs to be unit length.

This implies that only the direction matters and not the magnitude.
 
Thanks, so the reason why one projects the surface onto a plane like the xy-plane is to find how much of the different vector field components go trough the surface.
 
Liferider said:
Thanks, so the reason why one projects the surface onto a plane like the xy-plane is to find how much of the different vector field components go trough the surface.

In flux integrals its best to think of each point on your surface having its own normal vector at a point. On a plane, this doesn't change but on a curved surface it does.

What you are doing is just doing a projection of the 'flux component' with respect to the normal.

If the flux is parallel to the normal then the magnitude of the flux is at a maximum since it is going through the surface with maximum intensity. If the normal is perpendicular, then the flux will not even touch the surface resulting in a zero contribution since the flux is parallel to the surface itself.
 
The answer could be either "yes" or "no" depending upon exactly how you define the "normal vector". If you are given some vector function, [itex]\vec{v}(s,t)[/itex], defined over a surface F(s, t)= constant, to integrate the vector function over the surface by finding the gradient, [itex]\nabla F[/itex] which is, of course, normal to the surface.

Many texts form the unit normal, [itex]\vec{v}[/itex], by dividing that by the length [itex]\left|\nabla F\right|[/itex] but then form the "differential of surface area" [itex]dS= \left|\nabla F\right|dsdt[/itex]. But I have never seen much sense in dividing by [itex]\left|\nabla\right|[/itex] to get the unit normal, then multiplying by it to get the differential of surface area! Instead, I prefer to define the "vector differential of surface area", as done in many other texts, [itex]\vec{dS}= \nabla F dsdt[/itex].

On the one hand you can calculate the flux as
[tex]\int \vec{v}\cdot\vec{n}dS= \int \vec{v}\cdot\vec{n} \left|\nabla F\right| dsdt[/tex]
or as
[tex]\int \vec{v}\cdot\vec{dS}= \int \vec{v}\cdot\nabla F dsdt[/tex]

I prefer the second but they are equivalent.
 

Similar threads

  • · Replies 1 ·
Replies
1
Views
3K
  • · Replies 2 ·
Replies
2
Views
3K
  • · Replies 1 ·
Replies
1
Views
3K
  • · Replies 3 ·
Replies
3
Views
2K
  • · Replies 3 ·
Replies
3
Views
2K
  • · Replies 5 ·
Replies
5
Views
4K
  • · Replies 3 ·
Replies
3
Views
4K
  • · Replies 3 ·
Replies
3
Views
2K
  • · Replies 1 ·
Replies
1
Views
2K
Replies
7
Views
3K