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Airplane turns



 
 
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  #1  
Old April 17th 04, 01:29 AM
William W. Plummer
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"Teacherjh" wrote in message
...
To add to this answer (about how an airplane behavs during turns), most
airplanes are designed with dihedral. This means that the wings point up

a
little bit. If you looked at a plane from in front of the nose, the wings

will
form a slight V shape. This makes the "lift" that each wing produces

point a
little bit inward, towards the center of the plane, rather than straight

up.
Now, if the plane goes into a shallow bank, the wing that is lowered will
become more level, and the lift will point straight up, while the wing

that is
raised will become more tilted, and the lift will point more towards the

center
of the plane. More of the lift on this "tilted" wing is "wasted" (in the

sense
of not holding the airplane up). So, since the other wing exerts more

upwards
force, it causes the plane to return to level flight. This is one of the
things that makes an airplane inherently stable in flight.

Separate from this, when an airplane is banked in coordinated flight and
turning, the outer wing (which is the one that is raised to bank the plane

to
make the turn) is actually travelling faster than the inner wing. It has

to,
because that wing is further from the center of the turn. (to see this,
imagine the plane turning so sharply that it's just about pivoting on one
wingtip) The faster wing will produce more lift, and cause the airplane

to
bank in the direction of the turn. This is called "overbanking tendency".

So, there are two opposite tendencies. Dihedral is more important with

shallow
banks (and gentle turns), and the overbanking tendency is more important

with
steeper turns and banks. Somewhere in the middle, they cancel out.


Looking at the nose of the plane, we see the V-shape of the wings, the
dihedral angle. Lift is always perpendicular to the wings. So in flight,
the two lift vectors tilt in and "cross" over the plane itself. In level
flight the horizontal components of the two lift vectors are equal and
opposite. Thus, they cancel and the plane flies straight. Now, if you
bank the plane so that one wing is horizontal, that wing will have no
horizonal lift vector component. But, the other wing will have double. The
result is a big, net horizontal force on the plane. This forces the plane
to the center of the turn the way the force in a string swinging a rock
keeps the rock in a circle. That's what makes a plane able to go in a
circle, not the rudder.



  #2  
Old April 17th 04, 02:45 AM
Teacherjh
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Now, if you
bank the plane so that one wing is horizontal, that wing will have no
horizonal lift vector component. But, the other wing will have double. The
result is a big, net horizontal force on the plane. This forces the plane
to the center of the turn the way the force in a string swinging a rock
keeps the rock in a circle. That's what makes a plane able to go in a
circle, not the rudder.


Not quite. This does not change the direction of the nose, which is essential
for turning. By itself, what you post would lead to a slip. The plane would
travel in a straight line, at some angle to the nose.

Jose

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  #3  
Old April 17th 04, 03:59 AM
Peter Gottlieb
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"Teacherjh" wrote in message
...

Now, if you
bank the plane so that one wing is horizontal, that wing will have no
horizonal lift vector component. But, the other wing will have double.

The
result is a big, net horizontal force on the plane. This forces the plane
to the center of the turn the way the force in a string swinging a rock
keeps the rock in a circle. That's what makes a plane able to go in a
circle, not the rudder.


Not quite. This does not change the direction of the nose, which is

essential
for turning. By itself, what you post would lead to a slip. The plane

would
travel in a straight line, at some angle to the nose.


I guess this confuses me a bit. Maybe I'm tired and my brain confuses
easily.

Isn't it the case, in an earth-centric reference frame, that an object
moving in a straight line, when subjected to a horizontal force
perpendicular to that motion, will move in a circle?


  #4  
Old April 17th 04, 04:45 AM
Greg Esres
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when subjected to a horizontal force perpendicular to that motion,
will move in a circle?

In a sideslip, lift is perpendicular to the longitudinal axis of the
aircaft, not the direction of motion.

  #5  
Old April 17th 04, 01:25 PM
Teacherjh
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Isn't it the case, in an earth-centric reference frame, that an object
moving in a straight line, when subjected to a horizontal force
perpendicular to that motion, will move in a circle?


If the force is in fact perpendicular to the MOTION (the course) and not to the
HEADING. In the case of simply banking, the nose does not move (so the heading
remains the same) while the course changes (due to the force you are talking
about). But so long as the nose does not change direction, the force will not
change direction either and the plane will simply continue in a straight line,
in a slip.

(Actually, if you simply bank the plane (with alerons), the nose will tend to
move in the =opposite= direction, because of the drag induced by the alerons.
If your plane uses spoilers, the reverse is true)

Jose

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  #6  
Old April 17th 04, 04:02 PM
Peter Gottlieb
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"Teacherjh" wrote in message
...

Isn't it the case, in an earth-centric reference frame, that an object
moving in a straight line, when subjected to a horizontal force
perpendicular to that motion, will move in a circle?


If the force is in fact perpendicular to the MOTION (the course) and not

to the
HEADING. In the case of simply banking, the nose does not move (so the

heading
remains the same) while the course changes (due to the force you are

talking
about). But so long as the nose does not change direction, the force will

not
change direction either and the plane will simply continue in a straight

line,
in a slip.



I'm having a hard time wrapping my brain around this. Maybe the different
reference frames are confusing me.

Let's say I put the plane into a 30 degree bank with ailerons yet maintain
neutral rudder. To simplify things let's say I do this instantaneously.
Right at that moment, the nose is pointing in the original heading. But
what happens as this fairly large (earth referenced) horizontal lift force
acts on the plane; clearly it moves it sideways. But what happens to the
heading, that is messing me up. If the force continues, either it results
in an acceleration which causes increasing velocity or it reaches a terminal
velocity where the force is balanced by drag. Does the slip result in such
large drag so quickly that the net result is similar to a crosswind, or does
the plane act in the medium it is flying in (of course ignoring the earth
below) and have the nose indeed change heading because the plane is now
"climbing" sideways? I know from experience I need a lot of *opposite*
rudder to counteract a 30 degree bank and keep the nose on the same heading
(as in crosswind landings).


  #7  
Old April 17th 04, 05:51 PM
Teacherjh
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Let's say I put the plane into a 30 degree bank with ailerons yet maintain
neutral rudder. To simplify things let's say I do this instantaneously.
Right at that moment, the nose is pointing in the original heading. But
what happens as this fairly large (earth referenced) horizontal lift force
acts on the plane; clearly it moves it sideways. But what happens to the
heading, that is messing me up.


The heading does not change. The force is pushing the aircraft sideways.

Well, ok, the vertical tail will encounter some (sideways) resistance, causing
the plane to weathervane a bit into the wind and changing the heading too, but
that effect is small for small banks.


If the force continues, either it results
in an acceleration which causes increasing
velocity or it reaches a terminal
velocity where the force is balanced by drag.


The latter, ultimately. And yes, the plane is then "climbing" sideways. Part
of the reason for the heading change you would fight is the tail, which
produces down lift, keeping the nose up against gravity. When banked, this
results in a turn. But then less is available to keep the nose up, which is
why you apply back pressure on the elevators.

So all these things are interdependent, and become more so as the amount of
bank is increased.

Taken to the extreme (an aerobatics pilot might chime in here), if the wings
are vertical (a knife edge) the only thing keeping the airplane up is the
(once) vertical stabilizer and the fuselage. The (once) horizontal tail will
want to keep the nose "up", which is sideways, and the plane will want to turn
(do a loop horizontally). Ignoring other effects, of course.

Jose

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  #8  
Old April 17th 04, 06:01 PM
G.R. Patterson III
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Peter Gottlieb wrote:

Let's say I put the plane into a 30 degree bank with ailerons yet maintain
neutral rudder. To simplify things let's say I do this instantaneously.
Right at that moment, the nose is pointing in the original heading.


In my aircraft, the nose would swing in the opposite direction to the bank. The plane
would continue to fly the original heading. Sideways.

George Patterson
This marriage is off to a shaky start. The groom just asked the band to
play "Your cheatin' heart", and the bride just requested "Don't come home
a'drinkin' with lovin' on your mind".
 




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