An excellent way for students to gain a feel for aerodynamic forces is to fly a kite. The motion of the kite through the air is the result of forces being applied to the kite. The kite responds to these forces according to Newton's laws of motion. When the kite is in cruising flight you will notice that the control line produces a gentle curve from the hand of the flyer to the kite; the line sags under its own weight.

Mathematical equations have been developed which describe the shape of
the control line and we will now discuss these equations.
A co-ordinate system has been established with the **X** axis along the
ground, the **Y** axis perpendicular to the ground; the origin
is the hand of the kite flyer.
The kite is subjected to four main forces; the
lift **L**, the
drag **D**, the
weight **W**, and the
tension **T** in the control line.
The control line has a certain length **s** and the weight of the
control line is evenly distributed along the length at **p** ounces
per foot of line. The total weight of the control line is designated
**g** and

g = s * p

Because the weight of the control line is evenly distributed along the length, the line hangs under its own weight. A differential equation describes the transmission of the forces along the control line. (The math involved in the derivation and solution of this equation is taught in second year calculus classes.) Solving the differential equation, we can relate the shape of the control line (Y versus X) to the distribution of the tension in the control line. The resulting equation is shown in the red box at the top of the page.

Y = C2 + (D/p) * cosh [(p/D) * X + C1]

**C1** and **C2** are called constants of integration and must be determined at
the boundaries of the problem. The symbol **cosh** indicates the *hyperbolic
cosine* function. This is just a tabulated function, like the trigonometric
cosine, sine, and tangent, but with different values for a given input. There
is also a hyperbolic sine, **sinh**, and a hyperbolic tangent, **tanh**,
which we won't need for this problem.
The equation in the red box is called a **Catenary** and was developed
many years ago to describe cables hanging under their own weight. Other examples
would include telephone wires, cables on a suspension bridge, and even a jump
rope!

To solve for C1 and C2 we first use the boundary condition that at X=0, Y=0. Plugging X=0 into the catenary equation gives a relationship between the two constants

C2 = -(D/p) * cosh (C1)

So if we can determine C1, we now know C2. To get C1 we note that at the origin (X=0) the slope of the control line (dY/dX) is equal to the ratio of the component forces.

At X=0, dY/dX = (L - g - W) / D

The derivative of the cosh is the sinh. Plugging in X=0 gives the equation:

C1 = sinh^-1[(L - g - W) / D ]

where **sinh^-1** indicates the *inverse hyperbolic sine* of the expression.
That just means that the sinh(C1) is equal to (L - g - W) / D. There are also
tables of inverse hyperbolic sines, just like there are tables of inverse sines
in trigonometry.
With this value of C1 and the other equation to get C2 as a function of C1, we
now know the equation of the entire length of the control line.

At X=XK, dY/dX = (L - W) / D

We can use this information to determine the length **XK** for a given length
of string **s**. This equation is given at the bottom:

XK = (D / p) * [sinh^-1((L - W) / D) - C1]

The dependence on **s** is hidden in the constant **C1**. We could instead write:

XK = (D / p) * [sinh^-1((L - W) / D) - sinh^-1((L - W - p*s)/D)]

If we then plug this value of **XK** into the catenary equation, we can solve for the
height **Y** at which the kite is flying above the ground. Notice that the
shape of the line is not a straight line, so we can not use trigonometry to
get the height for a given length of line.

Enjoy flying ... but always fly safely.

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 *