NOC:Introduction to Airplane Performance


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.