1. AIRCRAFTS An aircraft is a machine which can derive its
support in the atmosphere from the reaction of air against earth
surface, either heavier or lighter than air which includes balloons
(fixed or free), airships, kites, gliders and other flying
machines.
2. AIRCRAFTS Aerostates Aerodynes Lighter than air. Aerostat is
a craft that remains aloft primarily through the use of buoyant
lighter than air gases, which impart lift to a vehicle with nearly
the same overall density as air hot air balloons. Heavier than air.
Any heavier-than-air craft that derives its lift in flight chiefly
from aerodynamic forces, such as the conventional airplane, glider,
or helicopter. e. g.- airships.
3. AERODYNES Fixed dynes Rotor dynes The wings are fixed and
hence called FIXED WING AIRCRAFTS. The wings are rotary and hence
called ROTOR WING AIRCRAFTS.
4. FIXED WING AIRCRAFTS Powered aircrafts Unpowered aircrafts
Unpowered aircraft are a group of aerial vehicles that can fly
without onboard propulsion. They can be classified as gliders,
balloons and kites. A powered aircraft is an aircraft that uses
onboard propulsion with mechanical power generated by an aircraft
engine of some kind. Aircraft propulsion nearly always uses either
a type of propeller, or a form of jet propulsion. Other potential
propulsion techniques such as ornithopters are very rarely
used.
5. Fixed wing aircrafts A fixed wing aircraft, typically called
an aeroplane, airplane or simply plane, is an aircraft, capable of
flight using forward motion that generates lift as the wing moves
through the air. Most fixed wing aircrafts are flown by a pilot or
board the aircraft, but some are designed to be designed remotely
or computer controlled.
6. Fixed wing aircrafts based on sets of wing According to sets
of wing, fixed aircrafts are of three types. a) Monoplane b)
Biplane c) Tri plane
7. MONOPLANE o A monoplane is a fixed wing aircraft of one main
set of wing surface.
8. BIPLANE A biplane is a fixed wing aircraft with two main
wings stacked one above other.
9. Triplane A tri plane is a fixed wing aircraft equipped with
three vertical stacked wing surfaces.
10. Types of fixed wing aircrafts based on position of wing
According to position of wing fixed wing aircrafts are of three
types. a) Low wing aircrafts b) Mid wing aircrafts c) High wing
aircrafts
11. Low wing aircraft o This category is for aircrafts with the
wings mounted at the bottom or below the fuselage. Dihedral wing at
the lower position gives the aircraft more stability.
12. Mid wing aircrafts This category is for aircrafts with the
wings mounted at the mid point of the fuselage.
13. High wing aircrafts This category is for the aircrafts with
the wings mounted above the fuselage. Anhedral wings gives the
aircraft less stability.
14. Aircrafts based on types of wing I. Straight wing II.
Tapered wing III. Elliptical wing IV. Sweep back wing V. Sweep
forward wing VI. Delta wing( triangular or arrow )
15. Aircrafts based on tail configuration a) T- tail b) H-tail
c) V-tail d) Canard design (horizontal tail plane is ahead of main
plane.) e) No tail( fly wing or delta wing. )
16. Motion of aircraft The aircraft has three axes such as A.
Longitudinal axis B. Lateral axis C. Normal axis or transverse axis
about these three axes it has six degrees of freedom.
17. PITCHING MOTION Nose up or nose down movement of the
aircraft is called pitching. It is a rotational motion of aircraft
about its lateral axis. The pitching motion is controlled by the
elevator. For operating the elevator there is a control stick
provided at the cockpit. Pitching is positive when nose up &
tail down and vice versa.
18. ROLLING MOTION It is a rotational motion of aircraft about
its longitudinal axis. During rolling ,one wing goes up and other
goes down. It is controlled by aileron. Rolling is positive when it
is clockwise negative when it is anti clock wise.( towards left
)
19. YAWING MOTION It is a rotational motion of aircraft about
the normal axis. The movement of aircraft towards right or left is
called yawing. It is controlled by rudder. Rudder deflects to right
, nose moves to left and tail moves to right.
20. AERODYNAMIC FORCES 1) WAIGHT- It is the force caused by the
gravitational attraction of earth. 2) LIFT- It is a mechanical
force generated by a solid object moving through a fluid. 3) DRAG-
It is the component of a resultant aerodynamic force which is
parallel to the motion of aircraft and act in the direction of
relative wind or opposite to the direction of motion of the
aircraft. 4) THRUST- It is a propulsive force which is generated to
make the aircraft moving forward.
21. FLAP These are the inward hinged portion of the wing
towards the trailing edge. They can only deflects downwards. In
some cases, they can be outward and rearward. Flaps are used or
deployed only during low speed flight to increase the lifting
capacity of the wing. It is a high lift device.
22. Aileron An aileron is a flight control surface usually
attached to the trailing edge of each wing of a fixed-wing
aircraft. Ailerons are used in pairs to control the aircraft in
roll, or movement around the aircraft's longitudinal axis, which
normally results in a change in heading due to the tilting of the
lift vector is a hinged .
23. Rudder A rudder is a device used to steer a aircraft that
moves through a medium (generally air or water). On an aircraft the
rudder is used primarily to counter adverse yaw and is not the
primary control used to turn the airplane. A rudder operates by
redirecting the fluid past the hull or fuselage, thus imparting a
turning or yawing motion to the craft. In basic form, a rudder is a
flat plane or sheet of material attached with hinges to the craft's
stern, tail, or after end. Often rudders are shaped so as to
minimize hydrodynamic or aerodynamic drag.
24. Elevons Elevons are aircraft control surfaces that combine
the functions of the elevator (used for pitch control) and the
aileron (used for roll control), hence the name. They are
frequently used on tailless aircraft such as flying wings. An
elevon that is not part of the main wing, but instead is a separate
tail surface, is a stabilator (but stabilators are also used for
pitch control only, with no roll function, as on the Piper Cherokee
series of aircraft). The word "elevon" is a portmanteau of elevator
and aileron.
25. Flaperons A flaperon is a type of aircraft control surface
that combines aspects of both flaps and ailerons. In addition to
controlling the roll or bank of an aircraft, as do conventional
ailerons, both flaperons can be lowered together to function
similarly to a dedicated set of flaps. Both ailerons could also be
raised, which would give spoilerons.
26. Ruddervators In aircraft, a V-tail (sometimes called a
Butterfly tail or spelled Vee-tail) is an unconventional
arrangement of the tail control surfaces that replaces the
traditional fin and horizontal surfaces with two surfaces set in a
V-shaped configuration when viewed from the front or rear of the
aircraft. The rear of each surface is hinged, and these movable
sections, sometimes called ruddervators, combine the tasks of the
elevators and rudder.
27. Aerofoil An aerofoil is the shape of a wing or blade (of a
propeller, rotor, or turbine) or sail as seen in cross-section. An
airfoil-shaped body moved through a fluid produces an aerodynamic
force. The component of this force perpendicular to the direction
of motion is called lift. The component parallel to the direction
of motion is called drag.
28. Types of aerofoil Semi-symmetrical Airfoil: Most of the
full size planes have this type installed. Its thinner than the
symmetrical airfoil and has lesser drag. It has a fully curved top
and a half curved bottom. Symmetrical Airfoil: They are curved on
both sides, equally. Generate high lifts with change in speed and
power. They are generally thick and hence are very strong. The
plane maintains its altitude with change in speed. Flat Bottom
Airfoil: Flat bottoms are usually seen in trainer flights. They
look extremely thin. Its bottom is flat and top is curved. Flat
bottom's are speed sensitive. They are similar to symmetrical
airfoils. When power and speed is added it produces great lift
Supersonic Airfoil: A supersonic airfoil is used to generate lift
at supersonic speeds. Its need arises when an aircraft is operated
consistently in supersonic range. Supercritical Airfoil: A
supercritical is designed to delay the drag in the transonic speed
rangeare a few to name. A supercritical is designed to delay the
drag in the transonic speed range. They have a flat upper surface,
a highly cambered aft and a greater leading edge radius.
29. Fuselage A fuselage is a long, thin body, usually with
tapered or rounded ends to make its shape aerodynamically smooth.
The fuselage may contain the flight crew, passengers, cargo or
payload, fuel and engines. The pilots of manned aircraft operate
them from a cockpit located at the front or top of the fuselage and
equipped with controls and usually windows and instruments. A plane
may have more than one fuselage, or it may be fitted with booms
with the tail located between the booms to allow the extreme rear
of the fuselage to be useful for a variety of purposes.
30. Structure of fixed wing Kites and some light weight gliders
and aeroplanes have flexible wing surfaces which are stretched
across a frame and made rigid by the lift forces exerted by the
airflow over them. Larger aircraft have rigid wing surfaces which
provide additional strength. Whether flexible or rigid, most wings,
have a strong frame to give them their shape and to transfer lift
from the wing surface to the rest of the aircraft. The main
structural elements are one or more spars running from root to tip,
and many ribs running from the leading (front) to the trailing
(rear) edge. Early aeroplane engines had little power and light
weight was very important. Also, early aerofoil sections were very
thin, and could not have strong frame installed within. So until
the 1930s most wings were too light weight to have enough strength
and external bracing struts and wires were added. When the
available engine power increased during the 1920s and 1930s, wings
could be made heavy and strong enough that bracing was not needed
any more. This type of unbraced wing is called a cantilever
wing.
31. Function of fixed wing A fixed-wing aircraft increases or
decreases the lift generated by the wings when it pitches nose up
or down by increasing or decreasing the angle of attack (AOA). The
roll angle is also known as bank angle on a fixed-wing aircraft,
which usually "banks" to change the horizontal direction of flight.
An aircraft is usually streamlined from nose to tail to reduce drag
making it typically advantageous to keep the sideslip angle near
zero, though there are instances when an aircraft may be
deliberately "sides lipped" for example a slip in a fixed- wing
aircraft .Fixed-wing transport aircraft are defined in terms of
their range capability as strategic airlift or tactical airlift to
reflect the needs of the land forces which they most often support.
These roughly correspond to the commercial flight length
distinctions needed.