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Course Co-ordinated by :
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NOC:Introduction to airplane performance (Video)
Modules / Lectures
General Introduction: Airplane Performance Characteristics
George Cayley: Concept of Lift and Drag
Introduction to airplane and its components
Hansa 3 Aircraft and its Primary Systems
Concept of Lift Aerofoil: Wing : Complete Aircraft
Standard Atmosphere: Description and Modeling
Measuring Instruments: Altimeter, Airspeed Indicator
Equations of Motion: Static Performance
Thrust Required, Power Required: Cruise
Excess Thrust and Power: Climb Angle and Rate of Climb
Thrust Required: A Closer Look
Modeling of CL: Dimensional Analysis
A Closer Look: Point Mass Model, Dimensional Analysis
Estimation of Drag Polar Through Flight Test
Estimation of Rate of Climb
Range and Endurance
Range and Endurance: Continued...
V stall: Cruise and Manoeuvre
Flaps:High Lift Devices to Reduce Take off / Landing Distance
Take off: Warm-up Lecture
Take off Performance
Take off Performance:Continued...
Landing Performance: Continued...
Challanges in Takeoff and Landing: Single and Twin Engines
Introduction to Static Stability
Positioning of Center of Pressure for Static Stability
Stability and Control: Designers Perspective
Stability and Control: Designers Perspective Continued...
Longitudinal Control: Elevator
Contribution of Wing and Tail: Stability
Stability: Wing and Tail Contribution
Control: Delta-e Required
Control: Delta-e Required continued...
Design Basics: Wing Loading & Thrust Loading
Design Basics: Sweep & Dihedral
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