Good

2. THE IMPORTANT PARTS OF AN AROPLANE
 WINGS
 FUSELAGE
 EMPENNAGE
 LANDING GEARS
 CONTROL SURFACE
 ENGINES

5. 1. CLASSIFICATION BY CONFIGURATION
 POSITION OF THE WING
 LOW WING
 MID WING
 HIGH WING
 NUMBER OF WINGS
 MONO PLANE
 BI PLANE
 TRI PLANE
 SHAPE OF THE WINGS
 DELTA WING
 DIAMOND WING
 SWEPT WING
 GULL SHAPED WING
 POSITION OF THE WINGS
 CONVENTIONAL WING
 NO TAIL OR TAILESS
 HORIZONTAL TAIL LOCATED AOVE THE VERTICAL TAIL
 CANARD TYPE

6. AIRCRAFT : CLASSIFICATION AND PARTS
2. LOCATION AND TYPE OF LANDING GEAR
 RETRACTABLE
 NON RETRACTABLE
 TAIL WHEEL
 NOSE WHEEL

7. AIRCRAFT : CLASSIFICATION AND PARTS
3. CLASSIFICATION BY POWER PLANTS
A. POWER PLANT TYPES
• PISTON ENGINE
• TURBO PROP
• TURBO SHAFT
• TURBO JET
• TURBO FAN
• ROCKET
B. NUMBER OF ENGINES
• SINGLE ENGINE
• TWO ENGINE
• MULTI ENGINE
C. LOCATION OF THE ENGINES
• NOSE
• FUSELAGE
• JET ENGINE SUBMERGED IN WING
• PYLON MOUNTING

8. AIRCRAFT : CLASSIFICATION AND PARTS
4. TYPES OF FUSELAGE
 ROUND
 SQUARE
 OVAL

9. AIRCRAFT : CLASSIFICATION AND PARTS
5. CLASSIFICATION BY PURPOSE
A. CIVIL
B. CARGO
C. MILITARY
I. BOMBERS
II. FIGHTERS
III. INTERCEPTORS

10.  PRIMARY GROUP
 AILERON
 ELEVATOR
 RUDDER
 SECONDARY GROUP
 TRIM TAB
 SPRING TAB
 AUXILIARY GROUP
 WING FLAPS
 SPOILERS
 SPEED BRAKES
 LEADING EDGE FLAP
 SLOTS

13. LONGITUDINALAXIS

14. LATERALAXIS

15. LATERALAXIS

17.  Longitudinal axis extends lengthwise from the nose through
the tail. Movement about the longitudinal axis is called
roll. Roll is controlled by the ailerons.

18. ELEVATOR
 Lateral axis extends crosswise from wingtip through wingtip.
Movement about the lateral axis is called pitch. Pitch is
controlled by the elevator.

19. RUDDER
 Vertical axis passes vertically through the center of gravity
(when the aircraft is in level flight). Movement about the
vertical axis is called yaw. Yaw is controlled by the rudder.

20. DIFFERENT TYPES OF AIRCRAFT ENGINES ARE
 PROPELLER WITH PISTON ENGINE
 JET ENGINE
• TURBOPROP
• TURBOFAN
• TURBOJET
• RAMJET
 ROCKET ENGINE

26. LIQUID FUEL
SOLID FUEL

27. AN AIRFOIL IS A SURFACE DESIGNED TO OBTAIN A
DESIRABLE REACTION FROM THE AIR THROUGH
WHICH IT MOVES
AIRFOIL GEOMETRY
• CHORD LINE
• MEAN CAMBER LINE
• ANGLE OF ATTACK
• ANGLE OF INCIDENCE

29.  DRAG IS THE RESOLVED COMPONENT OF
THE COMPLETE AERODYNAMIC FORCE
WHICH IS PARALLEL TO THE FLIGHT
DIRECTION (OR RELATIVE ONCOMING
AIRFLOW).
 IT MUST ALWAYS ACT TO OPPOSE THE
DIRECTION OF MOTION.
 IT IS THE UNDESIRABLE COMPONENT OF THE
AERODYNAMIC FORCE WHILE LIFT IS THE
DESIRABLE COMPONENT

31.  Weather conditions vary around the
globe, from day to day.
 Taking all these variations into design is
impractical.
 A standard atmosphere is therefore
defined, that relates fight tests, wind
tunnel tests and general airplane
design to a common reference.
 This common reference is called a
“standard” atmosphere.

32. AIRCRAFT CONSTRUCTION

33. TRUSS

34. MONOCOQUE

35. SEMI MONOCOQUE

36. THANK YOU