05. Roll-Yaw Coupling

Roll-Yaw Coupling

In a coordinated turn, we can turn sideways by rotating our lift vector. This lets us turn without experiencing sideforce! This is a bit unintuitive, and in general lateral-directional motion is more complicated than longitudinal motion.

In particular, roll and yaw are physically coupled in a way that leads to more complex dynamics.

To understand this roll-yaw coupling, we need to think about how lift is generated.

The same plane viewed from above and behind. Here it's shown following a straight line path.

The same plane viewed from above and behind. Here it's shown following a straight line path.

Consider the plane shown above. This plane is flying in a straight line with zero yaw rate

What can you say about the speed of the air flowing over the left wing compared to the speed of the air flowing over the right wing?

SOLUTION: v_\text{left} = v_\text{right}

Now consider the same plane using only it's rudder to maintain a constant yaw rate (so this is not a coordinated turn).

As this plane flies in a circular trajectory, what can you say about the speed of the air flowing over the left wing compared to the speed of the air flowing over the right wing?

SOLUTION: v_\text{left} > v_\text{right}

The increased relative airspeed over the left wing causes the left wing to feel more lift than the right wing.

This increased lift will cause a rolling moment that will cause the plane to roll clockwise.

The takeaway message here: yaw and roll are physically coupled. This coupling is what underlies the "Dutch Roll" mode, which you'll learn more about later.