Mod-06 Lec-17 Example problems

Course Lectures

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

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• Mod-01 Lec-02 Basic aerodynamics

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• Mod-02 Lec-03 Equilibrium and stability

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• Mod-02 Lec-04 Static vs dynamic stability

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• Mod-03 Lec-05 Criterion for stability,Wing contribution

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• Mod-03 Lec-06 Horizontal tail contribution

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• Mod-03 Lec-07 Wing plus tail contribution

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• Mod-04 Lec-08 Static margin and CG limits

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• Mod-04 Lec-09 Fuselage contribution

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• Mod-04 Lec-10 Powerplant contribution

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• Mod-04 Lec-11 Power effects on neutral point

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• Mod-05 Lec-12 Elevator

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• Mod-05 Lec-13 Stick free stability, Most fwd CG location

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• Mod-05 Lec-14 Longitudinal stick force per 'g', Ground effect

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• Mod-06 Lec-15 Control requirement, Pull-up maneuver, Maneuver point

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• Mod-06 Lec-16 Elevator per 'g' , Maneuver point

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• Mod-06 Lec-17 Example problems

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• Mod-07 Lec-18 Lateral-Directional Stability Derivatives, Fuselage/Vertical fin contribution

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• Mod-07 Lec-19 Roll stability, Wing sweep effect, Rudder

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• Mod-07 Lec-20 Dihedral effect, Various contributions

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• Mod-07 Lec-21 Power effects, Roll control, Aileron

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• Mod-07 Lec-22 Example problems

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• Mod-08 Lec-23 Derivation of Translational Motion Equations

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• Mod-08 Lec-24 Derivation of Angular Motion Equations

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• Mod-08 Lec-25 Description of various forces and moments

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• Mod-08 Lec-26 Nonlinearities and Associated Aircraft Behavior

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• Mod-09 Lec-27 Small perturbation method, Linearization of equations

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• Mod-09 Lec-28 Aerodynamic force and Moment Derivatives

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• Mod-09 Lec-29 Contribution of Aircraft components to Aerodynamic Derivatives

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• Mod-09 Lec-30 Linear Model and Aircraft Dynamics Modes

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• Mod-10 Lec-31 Short Period, Phugoid(Lanchester's formulation)

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• Mod-10 Lec-32 Short period mode approximation

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• Mod-10 Lec-33 Flying and Handling Qualities, Cooper Harper Scale

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• Mod-11 Lec-34 Pure rolling motion, Pure yawing motion,Spiral approximation

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• Mod-11 Lec-35 Spiral, Roll, Dutch roll Mode approximations

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• Mod-11 Lec-36 Lateral directional Flying Qualities, Routh's Stability criterion

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• Mod-11 Lec-37 Stability in Steady Roll Maneuver

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• Mod-12 Lec-38 Wind Effect on Aircraft Pure Plunging Motion

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• Mod-12 Lec-39 Wind Profiles, Longitudinal Mode Response to Wind Shear

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• Mod-13 Lec-40 Stability control/Augmentation

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

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