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Induced drag is the unavoidable by-product
of lift and increases as the angle of attack increases. Remember,
the greater the angle of attack, up to a critical angle, the
greater the amount of lift developed and the greater the induced
drag. **Since there are two different ways that lift is
produced, there are also two different types of induced drag:
dynamic drag (Newtonian) and pressure drag (Bernoulli).**

First, let's consider **dynamic induced
drag**, shown in Figure 4-8. If you hold your hand out of the
window of a moving car, with the front edge tipped up at an angle
to the relative wind to give it an angle of attack, you will feel
a force pushing your hand back, but also slightly upward. In
other words, depending on the angle of attack, there will be a
force backward (induced drag) and a force upward (lift). The
amount of force in each direction will depend on the angle of
attack. If the angle of attack is small, the drag and lift are
comparatively small. Any increase in angle of attack, up to a
certain point, will increase drag and lift. However, at very high
angles of attack, approaching the stall point, lift will decrease
and the drag will overcome lift and thrust with an accompanying
loss of speed and attitude. If you were to hold your hand
vertical to the relative wind, the only force would be backward;
that is, all dynamic drag and no lift.

Now let's consider **pressure-induced drag**,
which can be divided into the two types. You will remember that
the thin layer of air over the upper surface of the wing will
break away from the wing at high angles of attack and that the
flow will become turbulent as the flow of air breaks away from
the wing. This turbulence results in pressure drag and loss of
lift. Turbulence and pressure drag also result from the flow of
air around the wingtip as the comparatively high-pressure air
under the wing flows over the wingtip to the low-pressure area on
top of the wing.

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