Lecture 1 - General Introduction: Airplane Performance Characteristics
Lecture 2 - George Cayley: Concept of Lift and Drag
Lecture 3 - Introduction to airplane and its components
Lecture 4 - Hansa 3 Aircraft and its Primary Systems
Lecture 5 - Concept of Lift Aerofoil: Wing : Complete Aircraft
Lecture 6 - Drag Polar
Lecture 7 - Revision
Lecture 8 - Standard Atmosphere: Description and Modeling
Lecture 9 - Measuring Instruments: Altimeter, Airspeed Indicator
Lecture 10 - Equations of Motion: Static Performance
Lecture 11 - Thrust Required, Power Required: Cruise
Lecture 12 - Excess Thrust and Power: Climb Angle and Rate of Climb
Lecture 13 - Review
Lecture 14 - Thrust Required: A Closer Look
Lecture 15 - Modeling of CL: Dimensional Analysis
Lecture 16 - A Closer Look: Point Mass Model, Dimensional Analysis
Lecture 17 - Estimation of Drag Polar Through Flight Test
Lecture 18 - Estimation of Rate of Climb
Lecture 19 - Revision.
Lecture 20 - Range and Endurance
Lecture 21 - Range and Endurance: (Continued...)
Lecture 22 - Gliding Flight
Lecture 23 - Accelerated Flight
Lecture 24 - V-n Diagram
Lecture 25 - Revision..
Lecture 26 - V stall: Cruise and Manoeuvre
Lecture 27 - Flaps:High Lift Devices to Reduce Take off / Landing Distance
Lecture 28 - Take off
Lecture 29 - Take off Performance
Lecture 30 - Take off Performance: (Continued...)
Lecture 31 - Revision...
Lecture 32 - Landing Performance
Lecture 33 - Landing Performance: (Continued...)
Lecture 34 - Challanges in Takeoff and Landing: Single and Twin Engines
Lecture 35 - Introduction to Static Stability
Lecture 36 - Positioning of Center of Pressure for Static Stability
Lecture 37 - Revision.....
Lecture 38 - Stability and Control: Designers Perspective
Lecture 39 - Stability and Control: Designers Perspective (Continued...)
Lecture 40 - Longitudinal Control: Elevator
Lecture 41 - Contribution of Wing and Tail: Stability
Lecture 42 - Stability: Wing and Tail Contribution
Lecture 43 - Control: Elevator
Lecture 44 - Control: Delta-e Required
Lecture 45 - Control: Delta-e Required (Continued...)
Lecture 46 - Design Basics: Wing Loading & Thrust Loading
Lecture 47 - Design Basics: Sweep & Dihedral
Lecture 48 - Revision.
