Secondary Index

 


Aerodynamics Index

Definitions

Aircraft Axis
CG definition
Define Up and Down
Define Pitch, Bank, Hdg
Define: Lift, drag, etc.

Define Power

 

Physics Review

Newton's First Law
Newton's Second Law
Newton's Third Law
Reaction = Lift
Reaction = Drag
Conservation of Energy
What is a Vacuum
Action at a Distance

The 4 Forces

Spotting Forces & Moments

Performance

Drag Overview
Induced Drag
Induced Drag Equation
Total Drag

Jet Climb Performance
Prop Climb Performance
Range Jet

Range Prop

Forces in a Turn


Misc

Pitch Controls
Roll Controls

Configurations

Definition of Aircraft Axis

An airplane is of course a three-dimensional shape, therefore it has three axis:

  1. Longitudinal Axis
  2. Lateral Axis
  3. Normal Axis

It is important to remember that these axis are defined relative to the airplane, NOT the earth, the air, or the direction of flight.

When the engineers design the airplane they give it a floor that they generally intend to be approximately level when the airplane is in cruise. Think of the floor as the basic reference for understanding the three axis. The longitudinal and lateral axis lie parallel to the floor. The Normal axis is perpendicular to the floor, like a post sticking out of the ground.

Center of gravity as Axis Reference Point

All the axis run through the center of gravity, by definition. As we learned in the physics review, if a force acts through the center of gravity it causes acceleration, but NO rotation. Therefore the C of G is a handy reference point to use in defining our axis system. This way we know that if a force acts along any of the three axis is will not result in a rotation moment, or conversely if a force acts anywhere other than along an axis it WILL cause a rotation moment.

You are probably more familiar with the earth's axis, which is also usually called the poles. The center of gravity of the earth is right at the center, where the molten core is.

In the simulation to the left drag the top half of the earth up to reveal the c of g. Notice also that the pole is really just one axis that passes through the c of g.

IMPORTANT: Visualize that when you break the earth into two hemispheres, as to the left, the dividing line (at the equator) is a flat plane, and the c of g lies at the center of that plane.

 

Now consider the airplane to the left. It has a normal axis which corresponds to the earth's poles.

Drag the top half of the airplane up to reveal the c of g. Try to visualize that the airplane could be cut exactly in half like this such that the top half weighs the same as the bottom half. (If the division doesn't seem right to you, remember that the bottom half has the wings, and they contain all the fuel.) Note that the division into top and bottom half is based on weight, NOT size. In the case of the earth the two halves are the same size, shape, and weight. In the case of the airplane it has heavy and light parts, so the top half is larger, but it weights the same as the bottom half.

You should visualize that the point of division between the two parts is a flat plane. This plane lies parallel to the floor of the airplane by definition. The center of gravity is a point on that plane. It is not at the center, it is at the balance point. I.E. if you took the top half and balanced it on a point it would balance right at the c of g point - ditto the bottom half, if you turned it upside down. (Note: the c of g is so far forward because the engine is so much heavier than the airframe.)

In the simulation to the left you can drag the front half of the airplane forward, and the aft part rearward along the longitudinal axis. The results is a front and back half that, as above, are of the same weight.

The front half is physically smaller because the engine is so much heavier than the thin aluminum that makes up the fuselage. But both halves weigh the same. Obviously the exact division point will change with the number of people onboard, the amount of fuel in the tanks, and the baggage.

The place where the division occurs is the c of g and there is a flat plane that divides the two halves. The normal axis lies in that plane and the c of g is a point on the plane.

Both the normal and lateral axis lie in this plane.

The Plane of Symmetry

The airplane to the left can be split into left and right halves - try it to see.

Unlike the other two axis this split results in two sides that are mirror images of each other (like the hemispheres of the earth shown above.) Consequently the flat plane that divides the two sides is called the plane of symmetry.

 

 

The picture to the left shows a rear view of the airplane. It can also be split into left and right symmetrical sides.

You can see that both the normal and and longitudinal axis lie in the plane of symmetry, while the lateral axis is perpendicular to the plane of symmetry. When we look at a side view of the airplane, such as the ones above you can think of the paper, or computer screen, as representing the plane of symmetry.

The plane of symmetry is important in aerodynamics because it contains the lift vector, and usually also the thrust and drag vectors. Now that we know about the three axis and the plane of symmetry we will next discuss the forces acting on the airplane and how they relate to these axis.