What Notion is about as Healthy as that a Rattlesnake makes a Pleasant Pet?

How about the idea that the purpose of the rudder is to steer the airplane around the corner? No way.

The rudder gives the pilot the means to combat the adverse yaw effect of the ailerons. This is what a coordinated turn is all about. That is why we use rudder on going into a turn and why we use rudder when coming out of a turn. If the ailerons had no adverse yaw a plane wouldn't need a rudder.

It would be great if a student pilot had a early and clear concept of what an airplane had a rudder for. Think of all the skidding and slipping it would eliminate. Think of the fatalities it would save.

Remember your steep turn training. It was easy to enter with slight rudder involvement. Recovering was another thing. 

Banking out of fast, low angle of attack flight into a steep turn there is not much adverse aileron yaw and the need for rudder is less. Unbanking out of slow, high angle of attack flight, there is much adverse aileron yaw and much need for rudder. Your correct response will prevent a "broken neck" so to speak.

There is only one way to get out of a steep turn quickly and safely. This is especially important if the recovery from the steep turn has begun to sour.

First, to reduce the angle of attack, let the stick or wheel come forward to unstall the wings and giving the ailerons less adverse yaw. This enables the wing to lift itself.

Second, now apply a lot of top rudder (left rudder in a right turn and vice-versa).

Third, begin to apply high aileron to roll the airplane out of the steep bank.

Lesson today, "Stick Forward" to reduce angle of attack.

Here's to flying safely!

Jim

Torque or Slipstream? - Left Turning tendency

The Real Reason

The left turning tendency occurs when the propeller pushes back a stream of air mass which spirals as it streams to the rear.

With its spiraling motion the air mass hits the vertical fin at a slight angle. This pushes the tail to the right and yaws the nose to the left. Heres where the fun begins.

The propeller hits a small particle of air mass at the right -hand side of the planes nose. The impact of the propeller sends it backwards  and downward along the right side of the fuselage where it crosses underneath the pilots seat to the left side of the fuselage where it flows upward (cork-screw) and backward along the left side of the tail. It is then ready to cross over the top of the tail back to the right side; but, it finds its path blocked by the tail fin. The air mass particle impacts the fin with a force and shoves the tail fin to the right.

At the same time, in the beginning, another air mass particle is caught by the propeller on the left side of the planes nose. The impact sends the air mass particle speeding backward along the left side of the fuselage  and slightly upward. It crosses over the top of the cockpit and flows downward and backward along the right side of the tail. It is then ready to cross underneath the tail back to the left side. But, it runs into a problem. There is no tail fin to block the air mass particle. It exerts no force on anything and flows away behind the plane.

The net result of these two circulating air mass particles is a resultant shove of the tail fin to the right and a yaw of the plane to the left.

In aircraft design the tail fin is set at a slight angle so to line it up with the actual line of direction of the air flow at the tail in cruising, level flight.  The true reason for off setting the tail fin is not to make a force but, rather, to keep a force from being made.

In slower flight, as the tightness of the spiral of the air mass particle increases, the sideways shove of force on the tail fin increases. If the design angle offset is not sufficient, the left turning tendency continues and you must hold right rudder.

In gliding flight this tendency doesn't appear because the propeller is not creating a slipstream. The offset built into the tail fin is not necessary and, in fact, yaws the nose of the aircraft to the right. The pilot, in a glide, now holds slight left rudder.

You could abolish the left turning tendency by putting as much tail fin underneath the tail as there is atop the tail. The problem is the tail fin underneath would interfere with the conventional landing gear of a tail dragger. New plane design, with tricycle landing gear, have allowed the tail fin arrangement mentioned above to appear in modern planes.

The H-tail is here and slanted engines have eliminated left turn tendencies that plagued older aircraft.

Power Control and Stabilty

Plane Stability - Plane Performance and Throttle Settings

What is your plane stability after you trim for a particular speed? A plane, with perfect stability, will maintain that speed whether the power if off or the power is increased. Right? 

Try this in actual flight at cruising speed in straight and level flight and you will discover what actually happens when you change the power setting. Cut the power and the typical plane will descend in a glide at a speed well above your cruising speed. The glide will steepen into a dive. Push the throttle wide open and the plane will settle on a different, slower speed as it climbs.

Just why does a plane speed up when you close the throttle and slow down when you open up the throttle? Seems contradictory to most pilots. 

Plane design and propeller blast is one reason. The tail surfaces ride in a place, on a plane, where the propeller blast hits them. In cruise mode, at a specific speed, the tail surfaces receive an extra wind in power on flight causing an extra down force on the tail surfaces. With power off that wind and extra force disappear. 

In designing a plane there is something called a thrust-line location involved in a planes development. It concerns the location of the propeller in relation to the rest of the airplanes design. Consider a Cessna, with a high wing, with its engine mounted low to provide good vision for a pilot. This design arrangement will cause a nosing up tendency when the pull of the propeller coupled with the backward pull of the high wings drag with power on. This effect disappears when the power is off.

A change in relative wind created by the wings at cruise speed with the power on and how it changes with power off. Remember that the tail surfaces reside in the downwash created by the surfaces of the wing while in flight. With power on, the propeller blast hits certain parts of the wing. These parts work in an extra sharp relative wind that sends an extra sharp downwash to the tail surfaces. This produces an extra down force on the tail surfaces. When the power is off this effect disappears too.

The effect becomes more pronounced the heavier and more powerful the plane. To a pilot the effect is important because under some conditions an airplane may want to stall it self. 

From a safety point of view this may occur during a go-around as you attempt to land when a plane attempting to take off the runway suddenly appears in front of your plane. 

If your plane, that cruises at 100 mph in straight and level flight, stalls at 45 mph and your approach speed is 70 mph after trimming properly you could stall the aircraft in a go-around. You open the throttle wide to climb away and re-enter the airport flight pattern. If you don't simultaneously re-trim or apply strong forward pressure on the stick the plane wants to climb like mad. It will climb into a power stall because you think the plane will climb at 70 mph. (no change in airspeed).  Instead, the plane will want to fly at 45 mph or less to quickly gain altitude. 

You must respond by applying strong forward pressure on the stick and/or re-trimming to lower the nose of your plane to a safe climbing attitude and the speed up to a safe 70 mph.

Each plane, in review, has a built in tendency to keep its own   angle of attack constant and to keep its speed constant regardless of how the the amount of power delivered by the plane may change. This is basic. This basic tendency is overcome by the effects of power on and off discussed. You, the pilot must be aware of these contrary tendencies and act accordingly.

Deer Season - A Tendency to "Hunt!"

A "Hunting" Tendency

Stability - static and/or dynamic. In the real world most planes have a tendency to hunt. If you let go of your planes controls it won't fly at a constant speed.

Instead, it oscillates up and down. Why?

The up and down flight path of an oscillating plane is an complicated interaction of speed changes, flight paths, directions of the relative wind, angles of attack, changing drags, changing propeller efficiencies, horsepower outputs, changing lifts and slight downward and upward g-loads.

All the above means the plane is trying to get back to its proper cruising speed and proper angle of attack. The plane "over controls" itself and doesn't quite succeed in steadying itself down after you released the controls.

Since your plane is trying to return to a proper cruising speed and angle of attack, the apparent unstable "hunting" doesn't mean the airplane itself is unstable.

If the airplane was actually unstable, in a dive it would continue to dive or it would stay in a climb until it stalled.

The plane is primarily stable. If an airplane can't steady itself it is dynamically unstable. The airplanes oscillations continue to increase in violence until the plane disintegrates. 

The majority of airplanes are dynamically stable where the oscillations become weaker and weaker. The presence of unstable air or other disturbances may prevent the dampening of the oscillations. 

Knowing the technical theory on "hunting" is not very important to a pilot. Stability is important to a pilot because of the way it affects the feel and behavior of the plane while he controls the plane. 

If the pilot is controlling the plane it will not oscillate. 

Tail of an Airplane - Misunderstood

Tail of an Airplane

The tail of an airplane is arranged to resist the diving tendency of a plane. It is not meant to hold the lighter end of an airplane up in the air while in flight.

The purpose of the horizontal fin of the tail is to hold it down. It is like a wing but set at a negative angle of attack so the air flow against the horizontal tail fin produces, in normal flight, a downward force.

The reason for this downward force is the tail operates in the downwash of air that flows off the upper surface of the wing.

You recall an airplane creates "lift" by pushing air mass downward that creates a force upward that equals the weight of the plane in level, cruising flight. The downwash flows down on the horizontal fin of the tail and pushes it down more than you realize.

You know, from just looking at a plane, the nose is heavier than the tail. The nose-heavy plane tends to "nose the plane down" while the horizontal tail stabilizer tends to "nose it up."

When you trim a plane for level flight at cruising speed the two forces exactly balance each other. That is exactly what we do when we trim a plane for a certain speed. We adjust the angle of the horizontal tail fin so, at the particular speed we want to achieve, the downward air mass force on the tail will exactly balance the downward pull of the force of gravity on the nose.