Module 1 :
Introduction to Fixed-Wing UAVs
Classification of UAVs
International Standard Atmosphere
Measurement of Flight Velocity and Altitude
Anatomy of a Fixed Wing Aircraft
Airfoil Nomenclature

Module 2 :
Pitot and Static Tube
Differential Pressure Sensor
Generation of Lift and Drag
Center of Pressure and Aerodynamic Center
Wing Planforms
Lifting Line Theory

Module 3 :
Flow over Airfoil
Flow over Finite Wing
Airfoil Data Interpretation
Cl vs Alpha, Drag Polar
Airfoil Selection Procedure
Aircraft Equations of Motion
Aircraft Cruise Performance

Module 4 :
Thrust Required Calculation
Power Required Calculation
Power Plants – Performance Parameters and Selection

Module 5 :
Aircraft Climb Performance
Engine Sizing
Aircraft Weight Estimation
Electric Propulsion Systems – Battery Sizing

Module 6 :
Wing Sizing
Wing Planform Selection
Flight Demonstration – Delta Wing UAV
Static Stability Concepts

Module 7 :
Longitudinal Stability Concepts

Module 8 :
Wing Contribution
Tail Contribution
Effect of Variation of Center of Gravity Location