Flight Dynamics II - Stability

Flight Dynamics II - Stability

nptelhrd via YouTube Direct link

Mod-01 Lec-01 Earth Atmosphere,Aircraft components,Aircraft nomenclature

1 of 41

1 of 41

Mod-01 Lec-01 Earth Atmosphere,Aircraft components,Aircraft nomenclature

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Flight Dynamics II - Stability

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  1. 1 Mod-01 Lec-01 Earth Atmosphere,Aircraft components,Aircraft nomenclature
  2. 2 Mod-01 Lec-02 Basic aerodynamics
  3. 3 Mod-02 Lec-03 Equilibrium and stability
  4. 4 Mod-02 Lec-04 Static vs dynamic stability
  5. 5 Mod-03 Lec-05 Criterion for stability,Wing contribution
  6. 6 Mod-03 Lec-06 Horizontal tail contribution
  7. 7 Mod-03 Lec-07 Wing plus tail contribution
  8. 8 Mod-04 Lec-08 Static margin and CG limits
  9. 9 Mod-04 Lec-09 Fuselage contribution
  10. 10 Mod-04 Lec-10 Powerplant contribution
  11. 11 Mod-04 Lec-11 Power effects on neutral point
  12. 12 Mod-05 Lec-12 Elevator
  13. 13 Mod-05 Lec-13 Stick free stability, Most fwd CG location
  14. 14 Mod-05 Lec-14 Longitudinal stick force per 'g', Ground effect
  15. 15 Mod-06 Lec-15 Control requirement, Pull-up maneuver, Maneuver point
  16. 16 Mod-06 Lec-16 Elevator per 'g' , Maneuver point
  17. 17 Mod-06 Lec-17 Example problems
  18. 18 Mod-07 Lec-18 Lateral-Directional Stability Derivatives, Fuselage/Vertical fin contribution
  19. 19 Mod-07 Lec-19 Roll stability, Wing sweep effect, Rudder
  20. 20 Mod-07 Lec-20 Dihedral effect, Various contributions
  21. 21 Mod-07 Lec-21 Power effects, Roll control, Aileron
  22. 22 Mod-07 Lec-22 Example problems
  23. 23 Mod-08 Lec-23 Derivation of Translational Motion Equations
  24. 24 Mod-08 Lec-24 Derivation of Angular Motion Equations
  25. 25 Mod-08 Lec-25 Description of various forces and moments
  26. 26 Mod-08 Lec-26 Nonlinearities and Associated Aircraft Behavior
  27. 27 Mod-09 Lec-27 Small perturbation method, Linearization of equations
  28. 28 Mod-09 Lec-28 Aerodynamic force and Moment Derivatives
  29. 29 Mod-09 Lec-29 Contribution of Aircraft components to Aerodynamic Derivatives
  30. 30 Mod-09 Lec-30 Linear Model and Aircraft Dynamics Modes
  31. 31 Mod-10 Lec-31 Short Period, Phugoid(Lanchester's formulation)
  32. 32 Mod-10 Lec-32 Short period mode approximation
  33. 33 Mod-10 Lec-33 Flying and Handling Qualities, Cooper Harper Scale
  34. 34 Mod-11 Lec-34 Pure rolling motion, Pure yawing motion,Spiral approximation
  35. 35 Mod-11 Lec-35 Spiral, Roll, Dutch roll Mode approximations
  36. 36 Mod-11 Lec-36 Lateral directional Flying Qualities, Routh's Stability criterion
  37. 37 Mod-11 Lec-37 Stability in Steady Roll Maneuver
  38. 38 Mod-12 Lec-38 Wind Effect on Aircraft Pure Plunging Motion
  39. 39 Mod-12 Lec-39 Wind Profiles, Longitudinal Mode Response to Wind Shear
  40. 40 Mod-13 Lec-40 Stability control/Augmentation
  41. 41 Mod-13 Lec-41 Autopilots, Automatic Landing System

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