B.Tech IV Year II Semester (R16)
Basic Concepts: Helicopter Configurations-Single Main Rotor/Tail Rotor Configuration, Tandem Rotors, Coaxial Rotors, Side-By-Side Rotors, Intermeshing Rotors; Main Rotor System-Fully Articulated, Semi-Rigid and Rigid Rotor Systems, Combination Rotor Systems, Swash Plate Assembly, Anti-Torque Systems-Tail Rotor, Fenestron, NOTAR; Helicopter Controls: Collective Pitch Control, Cyclic Pitch Control, Anti-Torque Pedals, Throttle Control
Fundamentals of Rotor Aerodynamics: Momentum Theory Analysis in Hovering Flight, Disk Loading and Power Loading, Induced Inflow Ratio, Thrust and Power Coefficients, Comparison of Theory with Measured Rotor Performance, Non-Ideal Effects on Rotor Performance, Figure of Merit, Induced Tip Loss, Rotor Solidity and Blade Loading Coefficients, Momentum Analysis in Axial Climb and Descent, Momentum Analysis in Forward Flight
Blade Element Analysis, Rotating Blade Motion: Blade Element Analysis in Hover and Axial flight, Forward Flight; Rotating Blade Motion-Introduction, Types of rotors, Equilibrium about the flapping hinge and lead-lag hinge, Equations of motion for a flapping blade, Blade feathering and the swash plate,
Helicopter Performance: Introduction, Hovering and Axial Climb Performance, Forward Flight Performance, Performance Analysis, Auto-Rotational Performance, Vortex Ring State, Ground Effect, Performance in Maneuvering Flight, Factors Influencing Performance Degradation
Aerodynamic Design of Helicopters: Introduction, Overall Design Requirements, Conceptual and Preliminary Design Processes, Design of the Main Rotor, Fuselage Aerodynamic Issues, Empennage Design, Role of Wind Tunnels in Aerodynamic Design, Design of Tail Rotors, Other Ant-Torque Devices, High-Speed Rotorcraft
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