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Course Description

Flight dynamics is the study of the performance, stability, and control of vehicles flying through the air or in outer space.

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Course Syllabus
  • 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
  • Mod-13 Lec-41 Autopilots, Automatic Landing System

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