Flight Dynamics II (Stability)

Flight Dynamics II (Stability)
Flight Dynamics II (Stability) by Prof. Nandan Kumar Sinha, Department of Aerospace Engineering, IIT Madras. For more details on NPTEL visit http://nptel.iitm.ac.in
Mod-01 Lec-01 Earth Atmosphere,Aircraft components,Aircraft nomenclature
Mod-01 Lec-02 Basic aerodynamics
Mod-02 Lec-03 Equilibrium and stability
Mod-02 Lec-04 Static vs dynamic stability
Mod-03 Lec-05 Criterion for stability,Wing contribution
Mod-03 Lec-06 Horizontal tail contribution
Mod-03 Lec-07 Wing plus tail contribution
Mod-04 Lec-08 Static margin and CG limits
Mod-04 Lec-09 Fuselage contribution
Mod-04 Lec-10 Powerplant contribution
Mod-04 Lec-11 Power effects on neutral point
Mod-05 Lec-12 Elevator
Mod-05 Lec-13 Stick free stability, Most fwd CG location
Mod-05 Lec-14 Longitudinal stick force per 'g', Ground effect
Mod-06 Lec-15 Control requirement, Pull-up maneuver, Maneuver point
Mod-06 Lec-16 Elevator per 'g' , Maneuver point
Mod-06 Lec-17 Example problems
Mod-07 Lec-18 Lateral-Directional Stability Derivatives, Fuselage/Vertical fin contribution
Mod-07 Lec-19 Roll stability, Wing sweep effect, Rudder
Mod-07 Lec-20 Dihedral effect, Various contributions
Mod-07 Lec-21 Power effects, Roll control, Aileron
Mod-07 Lec-22 Example problems
Mod-08 Lec-23 Derivation of Translational Motion Equations
Mod-08 Lec-24 Derivation of Angular Motion Equations
Mod-08 Lec-25 Description of various forces and moments
Mod-08 Lec-26 Nonlinearities and Associated Aircraft Behavior
Mod-09 Lec-27 Small perturbation method, Linearization of equations
Mod-09 Lec-28 Aerodynamic force and Moment Derivatives
Mod-09 Lec-29 Contribution of Aircraft components to Aerodynamic Derivatives
Mod-09 Lec-30 Linear Model and Aircraft Dynamics Modes
Mod-10 Lec-31 Short Period, Phugoid(Lanchester's formulation)
Mod-10 Lec-32 Short period mode approximation
Mod-10 Lec-33 Flying and Handling Qualities, Cooper Harper Scale
Mod-11 Lec-34 Pure rolling motion, Pure yawing motion,Spiral approximation
Mod-11 Lec-35 Spiral, Roll, Dutch roll Mode approximations
Mod-11 Lec-36 Lateral directional Flying Qualities, Routh's Stability criterion
Mod-11 Lec-37 Stability in Steady Roll Maneuver
Mod-12 Lec-38 Wind Effect on Aircraft Pure Plunging Motion
Mod-12 Lec-39 Wind Profiles, Longitudinal Mode Response to Wind Shear
Mod-13 Lec-40 Stability control/Augmentation