| Sl.No | Chapter Name | English |
|---|---|---|
| 1 | Lecture 1 : Earth Atmosphere, Aircraft components, Aircraft nomenclature | Download Verified |
| 2 | Lecture 2 : Basic aerodynamics | Download Verified |
| 3 | Lecture 3 : Equilibrium and stability | Download Verified |
| 4 | Lecture 4 : Static vs dynamic stability | Download Verified |
| 5 | Lecture 5 : Criterion for stability, Wing contribution | Download Verified |
| 6 | Lecture 6 : Horizontal tail contribution | Download Verified |
| 7 | Lecture 7 : Wing plus tail contribution | Download Verified |
| 8 | Lecture 8 : Static margin and CG limits | Download Verified |
| 9 | Lecture 9 : Fuselage contribution | Download Verified |
| 10 | Lecture 10 : Powerplant contribution | Download Verified |
| 11 | Lecture 11 : Power effects on neutral point | Download Verified |
| 12 | Lecture 12 : Elevator | Download Verified |
| 13 | Lecture 13 : Stick free stability, Most fwd CG location | Download Verified |
| 14 | Lecture 14 : Longitudinal stick force per 'g', Ground effect | Download Verified |
| 15 | Lecture 15 : Control requirement, Pull-up maneuver,Maneuver point | Download Verified |
| 16 | Lecture 16 : Elevator per 'g' , Maneuver point | Download Verified |
| 17 | Lecture 17 : Example problems | Download Verified |
| 18 | Lecture 18 : Lateral-Directional Stability Derivatives, Fuselage/Vertical fin contribution | Download Verified |
| 19 | Lecture 19 : Roll stability, Wing sweep effect, Rudder | Download Verified |
| 20 | Lecture 20 : Dihedral effect, Various contributions | Download Verified |
| 21 | Lecture 21 : Power effects, Roll control, Aileron | Download Verified |
| 22 | Lecture 22 : Example problems | Download Verified |
| 23 | Lecture 23 : Derivation of Translational Motion Equations | Download Verified |
| 24 | Lecture 24 : Derivation of Angular Motion Equations | Download Verified |
| 25 | Lecture 25 : Description of various forces and moments | Download Verified |
| 26 | Lecture 26 : Nonlinearities and Associated Aircraft Behavior | Download Verified |
| 27 | Lecture 27 : Small perturbation method, Linearization of equations | Download Verified |
| 28 | Lecture 28 : Aerodynamic force and Moment Derivatives | Download Verified |
| 29 | Lecture 29 : Contribution of Aircraft components to Aerodynamic Derivatives | Download Verified |
| 30 | Lecture 30 : Linear Model and Aircraft Dynamics Modes | Download Verified |
| 31 | Lecture 31 : Short Period, Phugoid(Lanchester's formulation) | Download Verified |
| 32 | Lecture 32 : Short period mode approximation | Download Verified |
| 33 | Lecture 33 : Flying and Handling Qualities, Cooper Harper Scale | Download Verified |
| 34 | Lecture 34 : Pure rolling motion, Pure yawing motion,Spiral approximation | Download Verified |
| 35 | Lecture 35 : Spiral, Roll, Dutch roll Mode approximations | Download Verified |
| 36 | Lecture 36 : Lateral directional Flying Qualities, Routh's Stability criterion | Download Verified |
| 37 | Lecture 37 : Stability in Steady Roll Maneuver | Download Verified |
| 38 | Lecture 38 : Wind Effect on Aircraft Pure Plunging Motion | Download Verified |
| 39 | Lecture 39 : Wind Profiles, Longitudinal Mode Response to Wind Shear | Download Verified |
| 40 | Lecture 40 : Stability control/Augmentation | Download Verified |
| 41 | Lecture 41 : Autopilots, Automatic Landing System | Download Verified |
| Sl.No | Language | Book link |
|---|---|---|
| 1 | English | Not Available |
| 2 | Bengali | Not Available |
| 3 | Gujarati | Not Available |
| 4 | Hindi | Not Available |
| 5 | Kannada | Not Available |
| 6 | Malayalam | Not Available |
| 7 | Marathi | Not Available |
| 8 | Tamil | Not Available |
| 9 | Telugu | Not Available |