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Newton's
first law of motion
states that every object will remain at rest or in uniform motion in a
straight line unless compelled to change its state by the action of
an external force.
In general, an external force produces both a translation and a rotation
of an object.
The translation is described by Newton's
second law of motion
applied to the
center of gravity, **cg**,
of the object.
In general, the external force is applied at some point other than the cg.
If the object is unconstrained, like an aircraft in flight, the object
rotates about the cg due to the applied
torque
about the cg.
*(If the external force is applied at the cg, there is no rotation of
an unconstrained object.) *
If the object is constrained at some point, called the **pivot**, the object
rotates about the pivot due to the torque about the pivot.
In **equilibrium, or balance**, there are no net torques about the pivot and
the object does not rotate.

In flight, a kite rotates about the bridle point which is the knot that attaches the control line to the bridle string. The kite rotates because of the torques generated by the weight and the aerodynamic forces. The equation which describes the torque about the bridle point is

T = - L * cos(a) * (yb - cp) - L * sin(a) * xb

- D * sin(a) * (yb - cp) + D * cos(a) * xb

+ W * cos(a) * (yb - cg) + W * sin(a) * xb

where **T** is the net torque with a positive torque being
in the clockwise direction.
The forces are:
**L**, the
lift,
**D**, the
drag,
and **W**, the
weight.
**a** is the
angle of attack
which affects the magnitude of the aerodynamic forces.
**Xb** and **Yb** are the co-ordinates of the
bridle point,
**cg** is the location of the
center of gravity
and **cp** is the location of the
center of pressure.
The values for the weight and the
geometric
variables are a constant for a particular design.
Therefore, the net torque about the bridle point is a function
of the angle of attack.

If we plot the net torque versus angle of attack for
several different designs we can determine the balance and stability of the design.
If we can determine an angle of attack which makes the net torque equal to zero,
we have a **balanced** condition and the kite will not rotate in flight.
If the plot for a given design does not cross the angle of attack axis,
the kite never achieves a balanced condition and will continuously rotate
about the bridle point. Plots of unbalanced designs never cross the angle of attack axis.
Plots of balanced designs cross the axis with the balance
point given by the point on the axis where the plot crosses.
But balancing the kite is only part of the design problem. In flight, the kite
experiences small changes in the angle of attack due to turbulence in the air.
If the torque increases with a slight increase in angle of attack, we have an
**unstable** condition. The increased torque causes the angle of attack to
increase, which causes more torque, which causes more angle of attack .. and the
kite rotates out of control.
On the other hand, if a small increase in angle of attack from the balance point
causes a negative torque, the kite will return to the balance point condition.
This condition is called a **stable** design; any change away from the
balance point creates a torque which automatically returns the kite to the
balanced condition. For a balanced, stable design, the torque versus angle
of attack plot must cross the angle of attack axis, and have a negative slope.

The mathematical equations involved with the forces and torques on a kite can be solved by using a computer program. You can use the KiteModeler program to further study how kites work and to design your own kites.

Navigation...

- Beginner's Guide to Aerodynamics
- Beginner's Guide to Propulsion
- Beginner's Guide to Model Rockets
- Beginner's Guide to Kites
- Beginner's Guide to Aeronautics

Go to...

- Beginner's Guide Home Page

*byTom
Benson
Please send suggestions/corrections to: benson@grc.nasa.gov *