LANDING
The skill task most frequently failed on glider pilot practical tests
is AREA IV, TASK Q, NORMAL AND CROSSWIND LANDING. It involves
demonstrating the ability to touch down at a predetermined location
and to stop within a specified distance from a specified point.
The ability to stop where one wants to is enhanced by being able to
touch down at the appropriate spot, so we will first examine touch down
accuracy.
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This involves selecting an aiming point some 150 to 200 feet
short of the intended touch down point. In our illustrations the aiming
point is shown as a red target. The point where the glider flight
path intersects the ground is shown as a blue X, and the actual
touch down point is shown as a green rectangle, approximately 150
feet beyond the blue X. If the aiming point is chosen correctly and
the glider is flown correctly, the aiming point and the point where
the flight path would intersect the ground will coincide. Since flying into
the ground is considered poor practice, the pilot should flare just
before reaching the aiming point and touch down farther down the landing
area.
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As long as the glider's flight path continues toward the aiming
point, the aiming point has no relative motion
within the field of view. It only appears to grow larger as it is
approached. If constant pitch attitude is maintained, the point will
move neither up nor down on the glider canopy. It is unlikely that the
pilot will have a large red target on the ground at the aiming point, so
it becomes necessary to develop the skill of selecting some ground
feature to use instead. Once the aiming point is chosen, the pilot should
concentrate on it rather than the touch down spot, until it is time to
flare.
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The absence of apparent relative motion of the point where the glider
flight path intersects the ground is because its angle below the
horizon is constant. This angle is shown in the illustration in
magenta. Because the horizon is always at eye level, a line to the
horizon is horizontal at any altitude.
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If the current flight path will result in landing long, the point where
the flight path intersects the ground will be beyond the aiming point.
The angle of the aiming point below the horizon will increase as the
glider approaches it and eventually flies over it.
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From the glider, this results in the aiming point appearing to move down
on the canopy or toward the glider. The glider will overfly anything
that has this apparent movement. To correct for this, the pilot must
steepen the glide path
until the aiming point becomes stationary on the canopy or no longer
appears to be moving toward the glider.
Making the glide path steeper means decreasing the glide ratio (L/D ratio)
which means increasing drag. There are at least three ways to do that.
The pilot can deploy spoilers/dive brakes, slip the glider, or increase
speed by diving at the aiming point. (If a glider has flaps but not
spoilers/dive brakes, the flap function in landing is essentially the
same as any other drag device.)
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Just diving at the aiming point is not a very practical solution because
dissipating the excess speed, once the glider flares in ground effect,
will carry the glider far beyond the intended touch down spot.
However, "The Joy of Soaring" advocates pointing the glider at the
aiming point and controlling speed with spoilers/dive brakes. Many
instructors prefer to think of controlling air speed with pitch and
use the spoilers/dive brakes to control glide path. The glider, of
course, only responds to the combination of pitch and spoiler/dive brake
without regard for what the pilot is thinking as he/she actuates the
controls. In extreme cases the pilot may need full spoilers/dive brakes
and forward slip as well to achieve the required glide path. In this
case it would seem more logical to assign speed control to pitch.
Since no one questions using pitch for glider speed control in
inter-thermal flight, consistency suggests that we assign speed control
to pitch and glide path control to spoilers/dive brakes and/or slips in
landing as well.
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If the current flight path will result in landing short, the point where
the flight path intersects the ground will be closer than the aiming point.
The angle of the aiming point below the horizon will decrease as the
glider approaches it.
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From the glider, this results in the aiming point appearing to move up
on the canopy or away from the glider. To correct for this, the pilot
must shallow the glide path
until the aiming point becomes stationary on the canopy or no longer
appears to be moving away from the glider.
To make the glide path shallower means increasing the glide ratio (L/D ratio)
which means reducing drag. Closing the
spoilers/dive brakes is the only way to make a significant improvement in
glide ratio, so it is good practice to plan to fly
the final approach with half spoilers/dive brakes. Speed changes are
not appropriate here since the pattern
speeds for most gliders are very close to their best glide speeds and
change in either direction will only steepen the glide path.
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This is another good reason for assigning speed control to pitch and
glide angle to spoilers/dive brakes. Attempting to stretch the glide
by pulling back on the stick never works and can be disastrous.
The correct selection and use of an aiming point is essential in all
landings. The task is further complicated when the pilot must also
contend with a crosswind, shown in the following illustrations as a
large blue arrow.
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Remembering that the glider knows only
performance relative to the air mass it is flying in, this illustration
shows what would happen if the pilot encountering a crosswind
maintained the heading that initially pointed the glider toward the
runway. The path of the glider within the air mass is shown in red.
Its path relative to the ground is shown in green.
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To compensate for the drift caused by the crosswind, the pilot must
alter the flight path through the air. One method for doing this is
called crabbing, in which the glider is moving somewhat sideways over
the ground.
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It involves pointing the glider into the wind at an
angle that produces the desired path over the ground. Once the glider
is established on this heading (and assuming a constant wind) the
controls are neutralized, and the glider continues in normal flight.
The path of the glider within the air mass is again shown in red.
The path over the ground, shown in green, is directly to the runway.
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An obvious problem with using crab to correct for a crosswind is that
the glider longitudinal axis must be aligned with the runway before
touchdown. All aviation texts address this need by saying that
the pilot must yaw the aircraft into alignment with the runway just as
it is touching down. In one examiner's experience, few pilots do this
very well because it is difficult to determine exactly when to
initiate the yaw. Instead, most switch to a side slip for crosswind
correction some time during final approach.
There is often confusion about the difference between a side
slip and a forward slip. There is no difference aerodynamically, and
many feel that the names should be reversed. Perhaps the best way to
keep the terminology straight is to relate the name to application.
If the slip is to correct for a crosswind it is a side slip. If it is
to steepen the glide path it is a forward slip.
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The flight path of the glider within the air mass during a side slip,
again shown in red, is identical to that used when crabbing, and
the path over the ground, shown in green, is also the same. In a slip
the glider is moving through the air sideways, in the direction of the
low wing.
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When executing the side slip it may be helpful to think of the controls
as if they were independent, even though they always do interact. In
this case, the aileron controls the glider's lateral position over
the runway or its extended center line. The rudder is used to keep
the glider longitudinal axis aligned with the runway. A change in one
will necessitate a change in the other, but the visual clues and the
corresponding corrective action can be separated.
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It would seem that recognizing when the glider is over the extended
runway centerline would be easy, but many pilots have trouble with
this task. One way to verify alignment is to note the angle between
the runway center line and the horizon. If the glider is over the
center line, the angle will be 90 degrees (i.e. the runway will be
perpendicular to the horizon). If it is not, the pilot
should correct by increasing bank in the direction the runway is
pointing until the 90 degree angle is achieved. Then it may be
necessary to continue with some wing down to maintain the position.
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A pilot could meet the requirements of TASK Q by using spoilers/dive
brakes and crabbing and never demonstrate a slip. The FAA closed that
loophole with AREA IV, TASK R, SLIPS TO LANDING. The first objective
in every task in the test standard requires that the applicant
exhibit knowledge of the elements related to the task, so let's take
a look at the elements related to slips.
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In both the forward and side slip the glider is moving in a straight
line at a constant speed. According to Newton that means that the
forces acting on the glider must be balanced. Most pilots learn in
lesson #1 that turns are caused by the "horizontal component of lift",
produced by banking the glider so that its wing lift is no longer
directed up. In a slip we prevent turning by yawing the glider in the
opposite direction from the bank. In so doing the fuselage is now
placed at an angle to the relative wind where it produces "lift" that
exactly offsets the horizontal component of wing lift. Because the
wing is a much more efficient airfoil than the fuselage, the fuselage
yaw angle needed to do this is three to four times greater than the
bank angle.
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That is fortunate for glider pilots because it allows for
a relatively large wind correction angle in a side slip before the
glider wing tip would touch the ground in landing.
Airspeed control is important during a slip, but the airspeed indicator
may not be reliable because the pitot/static sensors are not aligned
with the flight path. If the pilot notes the pitch attitude that
produces the desired pattern speed before the slip is initiated and
maintains that pitch attitude during the slip, the airspeed likely will
be close enough. During eighteen years of examining glider pilots,
none ever slipped too slowly. Many slipped too fast and usually
overshot their intended touch down spot because of doing so.
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Pilots need to understand the difference between slips, which are
useful and safe, and skids, which serve no useful purpose and can be
extremely dangerous.
In both cases the glider is moving somewhat
sideways through the air. In the slip it is moving toward the low
wing. If it moving toward the high wing or with wings level it is
skidding. If the glider stalls while skidding it will almost
certainly enter a spin. If this occurs at low altitude, perhaps by
skidding the turn to final approach, there will be insufficient
altitude to recover. In order to avoid even a momentary skid, pilots
should enter slips by first lowering the appropriate wing and follow
immediately with the corresponding rudder displacement. As the wing is
lowered, adverse yaw will move the glider nose in the correct direction
so initial rudder application is unnecessary.
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From the pilot's perspective the only difference between a side slip
to correct for a crosswind and a forward slip to steepen the glide
path is that the nose of the glider is not aligned with the runway in
the forward slip. The ailerons are still used to keep the glider over
the runway centerline, but the rudder is used to control the severity
of the slip, rather than runway alignment.
A maximum slip requires full rudder displacement. Any
further increase in the corresponding bank will result in a turning
slip, which can be
used safely in the turn from base to final if the amount of altitude
loss needed dictates doing so. Just as when crabbing, the pilot must
align the glider longitudinal axis with the runway before touching
down.
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As noted previously, if the pilot does not begin a flare a few feet
above the ground, the glider will crash at the spot where its flight
path intersects the ground. The flare is simply a maneuver to reduce
the glider's vertical speed to zero just as it touches the ground. It
is accomplished by increasing pitch, which results in trading airspeed
for a reduction in sink rate, but not so much that the glider starts
to climb. The pilot may also adjust the spoilers/dive brakes to vary
the sink rate and modify the touch down point. If the approach has been
flown correctly, careful coordination of pitch and spoilers/dive brakes
should result in a smooth touch down at the desired point.
Stopping within the specified area should also be easy if the glider
touched down at the correct point and at the correct speed. The pilot
has a lot more control over the roll out than one might think for an
aircraft with no power. Spoilers/dive brakes are very effective during
the early part of the roll out. If the pilot landed with partial
spoilers/dive brakes, closing them will have the same effect as adding
power in a taxiing airplane. Opening the spoilers/dive brakes further,
engaging the wheel brake, and dropping the skid if the glider has one,
all can be used to shorten the roll out.
© 2000 Jim D. Burch 602-942-2734
jdburch@worldnet.att.net
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