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Part 2 –
Introduction 02
How to get the air to move over a wing?! 03
Basic aerodynamics 04
Generating Thrust 05
Generating Drag 07
Generating Lift 08
Take-off & Landing 10
Gliding flight in birds 11
Flapping the wings 12
References 16
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First of all; there’s what the birds and planes do to lift off the ground
and fly:
Blowing fast moving air above
the wing lowering the air
pressure above the wing.
Now, the air pressure under the
wing is higher and creates lift.
Lift does exactly what it sounds
like; it lifts the objects off the
ground when everything is just
right.
Then; to make the air moves faster, we should blow air over the top
to create the lower pressure.
Both birds and planes can’t do this. Instead; the wings of both are
shaped so that the air flew over the top of the wing a longer distance
and so it has to speed up as it goes over the top of the wing. This
creates the pressure difference above and under the wing.
(Streamlined shape wings).
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How to get the air to move over a wing?!
Getting the air to move over and under the wing also requires the
wing to be moving. This is called Thrust. Thrust is created when birds
flap their wings using there strong breasts muscles, while planes uses
their engines to generate thrust.
For both Birds and planes, thrust is the other part of creating lift and
the ability to fly.
Then, the shape of the wing and the ability to move it through the air
are the two things needed for flight.
Birds use their strong breast muscles to flap their wings and give
them the thrust to move through the air and fly.
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Basic aerodynamics
When a wing moves forward through still air, the air exerts a force on the wing.
At a certain position for any wing, when the wing is approximately parallel to
the air stream, no lift is generated; the force is entirely drag force. This is known
as ‘parasitic drag’, and other parts of the bird’s body will also make their own
contribution to the total parasitic drag. For the moment we shall ignore this
force.
Parasitic drag is drag that results when an object is moved through a fluid medium
(in the case of aerodynamics, a gaseous medium, more specifically, the atmosphere). Parasitic
drag is a combination of form drag, skin friction drag and interference drag.
The line down the center of the wing in this position is known as the ‘line of
zero lift’.
Now, if the wing is inclined to the air stream at an angle of attack α (measured
with respect to the line of zero lift), a large force appears on the wing, F.
This force is resolved into two components: the lift FL (which is at right angles
to the flow of air) and the drag (known as ‘induced drag’) FID.
It is usual to express the lift FL in terms of a dimensionless constant called the
aerodynamic coefficient of lift, CL, by dividing the
force FL by the term (1/2 AW ρ v2). This takes into
account the area AW of the wing, the density ρ of
the air (equal to 1.3 kgm−3
at sea level) and the
velocity of the wing through the air, v.
Hence
Note: CL is constant; it varies critically with angle of attack. Within the laminar region
up to about, say, 15◦, CL is roughly proportional to α. Beyond the 15◦ the wing stalls and the lift drops rapidly. A graph of
(CL) against α, though the precise details will depend crucially on the shape and construction of the wing.
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Generating thrust:
When a bird in cruising flight flaps its wings, the flow of air over the wing is no
longer horizontal. On the down stroke, the relative velocity between the air and
the wing is inclined upwards from below, while on the upstroke, the velocity of
the air is angled from above. Now, assuming
for the moment that the wing is symmetrical
and has zero angle of attack, it can be seen
from figure (4) that, on both the down stroke
and on the upstroke, the force of lift on the
wing (which is, by definition, at right angles
to the flow of air) is inclined forwards and has
a significant forward component.
This is the origin of the thrust produced by a
flapping wing. It is equally clear that, on
average, this wing will generate no lift, but
that is because the angle of attack is zero. I have, for simplicity, omitted the
induced drag here. We shall consider the drag forces later.
All that we require is that there shall be a net forward component of the lift.
Now what is the answer to the objection that, if the Strouhal angle is 22◦ or
more, the wing will stall on the down stroke? We must remember that a bird’s
wing rotates about the shoulder and that the Strouhal angle is measured at the
wingtip.
The angle of attack will therefore vary along the
wing from zero at the shoulder to a maximum of
22◦ at the tip. Most of the wing is still within the
acceptable range of attack angles. The problem
does, however, indicate that a vigorously flapping
wing is probably going to generate less lift and less
thrust than the theory would suggest. We can now
visualize the lift forces acting on a bird’s wing
during the down-stroke (figure 5).
Figure (4)
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As we move from the shoulder to the wing, the lift
increases in size and inclines further and further
forward. Since the angle of attack at the wing tip is
equal to the strouhal angle, the angle of attack α at a
distance r from the wing root can be obtained by a
certain equation.
In order to calculate the total forward thrust, we are
going to have to integrate along the length of the
wing from 0 to the semi-span of the wing for each
wing. We must also remember that the resultant of
the lift and drag forces inclines forward at an angle
of α/2, not α.
WING SPAN AND SEMI SPAN
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Generating Drag:
Drag is a force exerted on an object moving through a fluid; it is always
oriented in the direction of relative fluid flow (try running against a high wind
and you'll feel the drag pushing you back in the direction of relative fluid flow).
Drag occurs because the fluid and the object exchange momentum when
impacting, creating a force opposing the motion of the object.
The surface area of the object exposed to the fluid flow is higher.
The object is moving faster (or the relative fluid flow is faster).
The fluid has more momentum, or inertia (the viscosity and density of the
fluid are high).
This is generally low for air relative to other fluids such as water. Trying to
walk in a strong wind will demonstrate drag for you. A dropped weight falls
faster through air than through honey largely because of drag forces.
So, air causing drag on the flying bird, not only on the wings but also the body
and the tails of the bird.
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Generating lift
Of course, in order to fly straight at level, the wing must also produce a net lift.
It does this by using a positive angle of attack, β. On the down-stroke, this angle
is added to the α term, which governs the size of the lift force, but it does not
change its angle with respect to the vertical.
Also, since the vertical component of the lift force depends on the cosine of α,
we shall ignore this factor as α is small.
There is, however, the problem of whether or not the wing generates negative
lift on the upstroke. Mathematically we have tacitly assumed that the relation
between the coefficient of lift and the angle of attack works both for angles in
excess of 15º and for negative angles as well.
This is simply not the case. It is true that immense amounts of lift (and thrust)
are generated on the down-stroke, but it is inevitable that, on the upstroke, the
highly cambered wing of a typical bird is going to stall, and the forces
generated, both thrust and the - probably negative - lift, are going to be greatly
reduced.
When a large bird such as a heron with relatively slow wing beats flies closely
past, you can actually hear the powerful thrust of the down beat, but the
upstroke is relatively quiet. Many large birds partially fold their wings during
the upstroke, reducing both the area of the wing and, even more importantly, the
vertical speed of the wingtip.
Crows using an asymmetrical wing beat: a long powerful down-stroke followed
by a quick upstroke. This is further evidence that, in many situations, the forces
during the upstroke are considerably smaller than those involved in the down-
stroke.
Many soaring birds like gulls and birds of prey do not simply flap their wings
up and down but use an elliptical motion which carries the wing backwards
during the down-stroke and forwards during the upstroke. This changes little on
the down-stroke but significantly decreases the (negative) angle of attack on the
upstroke, possibly even reducing it to zero.
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The upshot of this discussion is that, in many cases, we can probably assume
that, for vigorous flapping, the formula we have derived work reasonably well
for the down-stroke but that a bird typically gains neither lift nor thrust during
the upstroke. The mean thrust and lift will therefore be approximately halved,
i.e.,
Take-off and Landing:
Take-off is one of the most energetically demanding aspects of flight, as
the bird needs to generate enough airflow across the wing to create lift. With
small birds a jump up will be sufficient, while for larger birds this is not
possible. In this situation, birds need to take a run up in order to generate the
airflow to take off. Large birds take off by facing into the wind, or, if they can,
by perching on a branch or cliff so that all they need to do is drop off into the
air.
The bird crouches and unfolds its wings. It jumps while its wings bite into
the air in a strong down-stroke.
The curved shape of the wing and its particular movement make flight
possible.
In down-stroke, the wing-beats push and compress the air underneath the
wings, adding air pressure there. The bird is thus thrust forward and upward.
Landing is also a problem for large birds with high wing loadings. This
problem is dealt with in some species by aiming for a point below the intended
landing area (such as a nest on a cliff) then pulling up beforehand. If timed
correctly, the airspeed once the target is reached is virtually nil. Landing on
water is simpler, and the larger waterfowl species prefer to do so whenever
possible, landing into wind and using their feet as skids. In order to lose height
rapidly prior to landing, some large birds such as geese indulge in a rapid
alternating series of sideslips or even briefly turning upside down in a maneuver
termed as whiffling.
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Gliding Flight in birds:
When a bird is gliding, it doesn't have to do any work. But it can't stay in the air
forever! The wings are held out to the side of the body and do not flap. As the
wings move through the air, they are held at a
slight angle, which deflects the air gently
downward.
Pushing the air downward causes a reaction force
in the opposite direction. You will notice a
reaction force, any time you push against
anything! The reaction force is called lift. Lift is a
force that acts roughly perpendicular to the wing
surface and keeps the bird from falling.
There is also air resistance or drag on the body and
wings of the bird. This force would eventually
cause the bird to slow down, and then it wouldn't
have enough speed to fly. To make up for this, the
bird can lean forward a little and go into a shallow
dive. That way, the lift force produced by the
wings is angled forward slightly and helps the bird
speed up. Really what the bird is doing here is
giving up some height in exchange for increased
speed. (To put it another way, it is converting its
gravitational potential energy into kinetic energy.)
The bird must always lose altitude, relative to the
surrounding air, if it is to maintain the forward
speed that it needs to keep flying.
In gliding flight, a bird's wings deflect air downward, causing a lift force that holds the
bird up in the air.
By tilting forward and going into a slight dive, the bird can maintain forward speed.
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Flapping the Wings:
Flapping of the wings creates forward thrust, while the air rushing against the
wings maintains lift.
There are three main movements in flapping flights:
1. Flap: up and down movements of the wing about the
shoulder joint.
2. Pitch: Rotating the wing along the span to change the
angle of attack.
3. Flex: Lengthening and shortening the wing.
Recall that the wings are angled slightly, which allows them to deflect the air
downward and produce lift. The slight angle of the wings is called the angle of
attack. If the angle of attack is too great, the wing will produce a lot of drag. If
the angle is too small, the wing won't produce enough lift. The best angle
depends on the shape of the wing, but it's usually just a few degrees! Notice that
what matters is the angle relative to the direction of travel, not relative to the
horizontal.
The wings flap with an up-and-down motion. This
may change in special situations, but we aren't going
to talk about those until later. When the wings move
up and down, they are also moving forward through
the air along with the rest of the bird. Close to the
body, there is very little up and down movement.
Farther out toward the wingtips, there is much more
vertical motion.
As the bird is flapping along, it needs to make sure it
has the correct angle of attack all along its wingspan.
Since the outer part of the wing moves up and down
more steeply than the inner part, the wing has to
twist, so that each part of the wing can maintain just
the right angle of attack. The wings are flexible, so
they twist automatically. This picture shows how the wing must twist in the
down-stroke, to keep each part of the wing aligned with the local direction of
travel.
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If thrust is produced in the down-stroke, you might be wondering what happens
in the upstroke.
Since the wing is travelling upward, shouldn't there be a lot of drag, tending to
slow the bird down?
To avoid this, the bird does two things:
The outer part of the wing points straight along its line of travel so it can
pass through the air with the least possible resistance. In other words, the
angle of attack is reduced to zero.
The bird partially folds its wings, which reduces the wingspan and
eliminates the draggy outer part of the wing. This is not strictly necessary
though, and most insects lack the capability.
The inner part of the wing is different.
There is little up-and-down movement
there, so that part of the wing continues
to provide lift and function more or less
as it would when gliding. Because only
the inner part of the wing produces lift in
the upstroke, the upstroke as a whole
offers less lift than the down-stroke.
As a result, the bird's body will bob up
and down slightly as the bird flies.
This control of the wing surface can
prevent flow separation and enhance lift to drag ratio.
The pressure of the air on top of its wings is less than the pressure below. When
the bird's wings move forward, the air must travel farther and faster over the
curved top surface of the wings than it does over the bottom surface. The
pressure on top of the wing is less than the pressure below, because of this
difference in the speed of the air.
Left: The wing feathers
overlap on the down-stroke
and push against the air. On
the upstroke, the feathers twist
open, allowing the air to pass
through and making it easier
to lift the wing.
Right: Air flowing over the top of a bird's wing decreases in pressure, but the air under the
wing maintains a constant pressure. This difference in air pressure helps lift the bird in flight.
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Dickinson [6] discovered that at the
onset of rotation, two vortices are
created.
One is a bound vortex attached to the
wing surface facing the direction of
rotation. The second vortex, termed
the ‘‘mirror vortex’’, is a free vortex
of equal and opposite strength to the bound vortex. This free vortex sheds from
the surface opposite the direction of rotation.
When the rotational motion ends, the bound vortex splits into two vortices that
shed from the leading and trailing edges.
Wing rotation created lift even at zero AOA and appeared to enhance
it for all other angles of attack tested.
If a wing translates through a series of vortices (such as a von Karman
street) created by the previous stroke, then it would encounter a high
velocity fluid stream that could speed the fluid velocity in the direction
of translation and add to lift production.
VORTICES ON WING SURFACE
VON KARMAN STREET
VORTEX
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And from here; it isn’t all about Birds Flying but a conclusion of the
aerodynamic and analysis of their property of flying.
And Allah who gave them this ability of flying and we notice that they are fully
designed as a perfect engineering design.
Attached below the references we laid onto for all of these information,
containing websites, published books by scientists or even biologists; because
these creatures aren’t include only engineering application but also science
explanations must be included.
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References:
[1] Ask a Biologist Website: Ask a Biologist began in 1997 in the School of
Life Sciences. It is designed as an educational resource for students, and their
teachers and parents. Ask A Biologist funded in part by the National Science
Foundation.
http://www.askabiologist.asu.edu
[2] The Physics of Flight by Oliver Linton.
[3] WIKIPEDIA. http://en.wikipedia.org/wiki/Main_Page
[4] Bird Flight Website. http://www.ornithopter.org/birdflight/
[5] Robinson Library. The Robinson ( A collector of books most of his life, and
his library currently contains over 3,000 books.) Library website was created as
a way to impart knowledge to anyone who seeks to broaden their world. The
idea is to provide information on as wide a variety of subjects as possible. And
its information are directly from books.
[6] Dickinson MH, Lehmann FO, Gotz KG. The active control of wing rotation by
Drosophila. J Exp Biol 1993;182:173–89.
[7] Liu H, Ellington CP, Kawachi K, Van den Berg C, Willmott AP. A computational
fluid dynamic study of hawkmoth hovering. J Exp Biol 1998;201:461–77.
[8] Van Den Berg C, Ellington CP. The three-dimensional leading-edge vortex of a
hovering model hawkmoth. Philos Trans R Soc London Ser B 1997;353:329–40.
Note: The reference name followed by its number
between brackets [].