AIRCRAFT BASICS 
Presented By- 
Yajnesh Chaturvedi 
Mgr. (D), ASERDC
Aircraft
Aircraft Structure
Wings
Wing (Contd.) 
• High-wing 
• Mid-wing 
• Low-wing 
• Monoplanes – one set of wings 
• Biplanes – two set of wings 
• Ailerons 
• Flaps
Empennage
Empennage (Contd.) 
• Vertical stabilizer 
• Horizontal stabilizer 
• Rudder 
• Elevator 
• Trim tabs
Landing Gear 
• Two main wheels and a third wheel at the 
front or rear 
• Parking,Taxiing, Take off, Landing 
• Wheels - common 
• Floats – water operation 
• Skis - snow
Power Plant
Power Plant (Types) 
• Pistonprop 
• Turboprop 
• Turbojet 
• Turbofan 
• Ramjet
Turbo Jet Engine
Single-spool Axial Flow Turbo Jet
Twin-spool By-pass Turbo-Jet
Ram Jet Engine
Lift, Thrust, Weight, and Drag
Bernaulli’s Equation 
First term is the internal energy of unit mass of the air, ½ v² is the kinetic energy 
of unit mass and gz is the potential energy of unit mass. Thus, Bernoulli’s 
equation in this form is a statement of the principle of conservation of energy in 
the absence of heat exchanged and work done. 
This is Bernoulli’s equation for an incompressible fluid, i.e. a fluid that cannot 
be compressed or expanded, and for which the density is invariable.
Aerofoil (Wing) Section
Air flow over an aerofoil inclined 
at a small angle
Pressure Distribution over Aerofoil
Lift Produced
Principal Aerodynamic Forces 
During Flight
Axes of an Airplane
Primary Flight Controls
Primary Flight Controls
Primary Flight Controls 
• Aileron 
• Elevator 
• T-tail 
• Canard 
• Rudder 
• V-tail
Pitch
Yaw
V-tail
Secondary Flight Controls 
• Flaps 
• Leading Edge Devices 
• Spoilers 
• Trim Devices
Flaps
Leading Edge Devices
Spoilers
Trim Systems 
• Trim Tabs 
• Balance Tabs 
• Anti-servo Tabs 
• Ground Adjustable Tabs 
• Adjustable Stabilizer
Trim Tabs
Anti-servo Tabs
Ground Adjustable Tabs
Adjustable Stabilizer

Aircraft basics