Flight Dynamics II (Stability) by Nandan Kumar Sinha (at IIT Madras)

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source: nptelhrd    2012年7月17日
Aerospace - 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 47:57
Lec-02 Basic aerodynamics 56:14
Lec-03 Equilibrium and stability 51:56
Lec-04 Static vs dynamic stability 41:50
Lec-05 Criterion for stability,Wing contribution 42:00
Lec-06 Horizontal tail contribution 52:34
Lec-07 Wing plus tail contribution 49:30
Lec-08 Static margin and CG limits 45:51
Lec-09 Fuselage contribution 49:23
Lec-10 Powerplant contribution 48:02
Lec-11 Power effects on neutral point 47:30
Lec-12 Elevator 41:21
Lec-13 Stick free stability, Most fwd CG location 47:40
Lec-14 Longitudinal stick force per 'g', Ground effect 44:14
Lec-15 Control requirement, Pull-up maneuver, Maneuver point 50:43
Lec-16 Elevator per 'g' , Maneuver point 49:39
Lec-17 Example problems 49:56
Lec-18 Lateral-Directional Stability Derivatives, Fuselage/Vertical fin contribution 50:12
Lec-19 Roll stability, Wing sweep effect, Rudder 48:40
Lec-20 Dihedral effect, Various contributions 44:57
Lec-21 Power effects, Roll control, Aileron 40:09
Lec-22 Example problems 51:13
Lec-23 Derivation of Translational Motion Equations 43:40
Lec-24 Derivation of Angular Motion Equations 50:57
Lec-25 Description of various forces and moments 42:40
Lec-26 Nonlinearities and Associated Aircraft Behavior 52:11
Lec-27 Small perturbation method, Linearization of equations 45:49
Lec-28 Aerodynamic force and Moment Derivatives 50:59
Lec-29 Contribution of Aircraft components to Aerodynamic Derivatives 52:23
Lec-30 Linear Model and Aircraft Dynamics Modes 52:05
Lec-31 Short Period, Phugoid(Lanchester's formulation) 48:27
Lec-32 Short period mode approximation 49:36
Lec-33 Flying and Handling Qualities, Cooper Harper Scale 48:15
Lec-34 Pure rolling motion, Pure yawing motion,Spiral approximation 50:10
Lec-35 Spiral, Roll, Dutch roll Mode approximations 48:54
Lec-36 Lateral directional Flying Qualities, Routh's Stability criterion 45:06
Lec-37 Stability in Steady Roll Maneuver 49:26
Lec-38 Wind Effect on Aircraft Pure Plunging Motion 47:14
Lec-39 Wind Profiles, Longitudinal Mode Response to Wind Shear 43:06
Lec-40 Stability control/Augmentation 44:32
Lec-41 Autopilots, Automatic Landing System 42:59

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