Lecture 1 - Introduction to Aeromechanics of Unmanned Aerial Systems
Lecture 2 - Introduction to Vertical Takeoff and Landing UAVs
Lecture 3 - Aerodynamics of Fixed Wing Aerial Vehicles: Concept of Lift and Drag
Lecture 4 - Basics of Aerodynamics
Lecture 5 - Basics of Aerodynamics and Flight Instruments
Lecture 6 - Concepts of Aerodynamics and International Standard Atmosphere
Lecture 7 - International Standard Atmosphere and Aircraft Equation of Motion
Lecture 8 - Thrust and Power Considerations for Fixed Wing UAVs
Lecture 9 - Flight Performance
Lecture 10 - Range and Endurance
Lecture 11 - Load Factor and V-n Diagram
Lecture 12 - Design philosophy for structures; Load factor in turning flight
Lecture 13 - Concepts of Stability; Introduction to Rotary Wing Systems
Lecture 14 - Elements of Rotary Wing Aerial Vehicles
Lecture 15 - Momentum Theory of Rotor / Propeller in hover
Lecture 16 - Momentum Theory of Propellers / Rotors in Climb
Lecture 17 - Operating States of Propeller
Lecture 18 - Inflow for Descending Flight and Edgewise Flight
Lecture 19 - Power for Rotor in Edgewise Flight and Blade Element Theory
Lecture 20 - Blade Element Theory and Momentum Theory
Lecture 21 - Blade Element Momentum Theory (BEMT)
Lecture 22 - Ideal Hovering Rotor and Mean Lift Coefficient
Lecture 23 - Prandtl Tip Loss Factor
Lecture 24 - Performance of Edgewise Rotor in Forward Flight - I
Lecture 25 - Performance of Edgewise Rotor in Forward Flight - II
