Use of the Biot Savart Law in Lifting Line theory

In summary, the Biot-Savart law is not limited to one plane and considers the contribution of all points along a vortex filament. This allows it to accurately predict the lift distribution along a wing, even though vortices are only generated at certain points. The law takes into account the cumulative effect of all vortices, resulting in an accurate representation of the lift distribution.
  • #1
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In deriving the lifting line theory Prandtl used the Biot-Savart Law - now from the definition of a vortex filament, it is a line where each point generates a vortex flow in the surrounding fluid. Considering a particular point, if the surrounding fluid is inviscid then shouldn't the vortex motion be restricted to only one plane, the plane perpendicular to the filament and passing through that point? If this is correct, then how can Biot-Savart law be applied where the effect of a small filament is felt everywhere?
 
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  • #2
The Biot-Savart law does not assume that a vortex filament has any particular orientation, and so is not restricted to one plane. The basic idea of the law is that the strength of the induced velocity due to a small filament is proportional to the strength of the vortex and the inverse square of the distance from the filament. The induced velocity field is then the sum of the effects of all the infinitesimal filaments. In practice, the Biot-Savart law is usually only applied in two dimensions, with the assumption that the third dimension can be neglected. This is a reasonable approximation for most problems in aerodynamics.
 
  • #3


I agree with your understanding of the vortex filament and its motion in an inviscid fluid. The Biot-Savart law can still be applied in this situation because it takes into account the contribution of all points along the filament, not just at a particular point. This is why the lifting line theory is able to accurately predict the lift distribution along the entire wing, even though the vortices are only generated at certain points on the wing. The Biot-Savart law takes into account the cumulative effect of all these vortices, resulting in an accurate representation of the lift distribution. I hope this helps clarify your understanding.
 

Related to Use of the Biot Savart Law in Lifting Line theory

1. What is the Biot Savart Law?

The Biot Savart Law is a fundamental principle in electromagnetism that describes the magnetic field produced by a current-carrying wire. It states that the magnetic field at any point in space is directly proportional to the current in the wire, the length of the wire, and the sine of the angle between the wire and the point.

2. How is the Biot Savart Law used in Lifting Line theory?

In Lifting Line theory, the Biot Savart Law is used to determine the lift and drag forces on a wing by calculating the induced velocity at each point along the wing using the formula V = (μ0 / 4π) * (I * dl * sinθ / r^2). This induced velocity is then used to calculate the lift and drag coefficients, which are essential in understanding the aerodynamics of a wing.

3. What are the assumptions made in using the Biot Savart Law in Lifting Line theory?

There are several assumptions made when using the Biot Savart Law in Lifting Line theory. These include assuming a steady flow, a constant angle of attack, and a constant circulation around the wing. Additionally, the law assumes that the wing is infinitely long and has a constant cross-sectional area.

4. What are some limitations of using the Biot Savart Law in Lifting Line theory?

One limitation of using the Biot Savart Law in Lifting Line theory is that it does not take into account the effects of viscosity, which can significantly affect the aerodynamics of a wing. Additionally, the law assumes an idealized wing shape and may not accurately represent the actual aerodynamics of a real wing.

5. Can the Biot Savart Law be used for any wing shape in Lifting Line theory?

No, the Biot Savart Law can only be used for wings with a constant circulation, such as elliptical, rectangular, and triangular wings. It cannot be applied to wings with varying circulation, such as swept or tapered wings. In these cases, more complex mathematical models must be used.

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