Flight Dynamics II (Stability) - Study24x7

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# Flight Dynamics II (Stability)

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Aircraft Dynamic Stability and Response deals with the fundamentals of dynamic stability in aircraft. Topics covered include flight dynamics, equations of motion, and lateral and longitudinal aerodynamic derivatives. Basic lateral and longitudinal motions are also considered. ...

• Total 13 Modules
• 41 Videos
• Published on 01 July, 2019

## Introduction to the course

• Lecture 1 : Earth Atmosphere, Aircraft components, Aircraft nomenclature

47m
• Lecture 2 : Basic aerodynamics

56m

## Equilibrium and stability

• Lecture 3 : Equilibrium and stability

51m
• Lecture 4 : Static vs dynamic stability

41m

## Longitudinal static stick fixed stability

• Lecture 5 : Criterion for stability, Wing contribution

42m
• Lecture 6 : Horizontal tail contribution

52m
• Lecture 7 : Wing plus tail contribution

49m

## Longitudinal stability and neutral point

• Lecture 8 : Static margin and CG limits

45m
• Lecture 9 : Fuselage contribution

49m
• Lecture 10 : Powerplant contribution

48m
• Lecture 11 : Power effects on neutral point

47m

## Longitudinal control

• Lecture 12 : Elevator

41m
• Lecture 13 : Stick free stability, Most fwd CG location

47m
• Lecture 14 : Longitudinal stick force per 'g', Ground effect

44m

## Longitudinal control and maneuverability

• Lecture 15 : Control requirement, Pull-up maneuver,Maneuver point?

50m
• Lecture 16 : Elevator per 'g' , Maneuver point

49m
• Lecture 17 : Example problems

49m

## Lateral directional static stability and control

• Lecture 18 : Lateral-Directional Stability Derivatives, Fuselage/Vertical fin contribution

50m
• Lecture 19 : Roll stability, Wing sweep effect, Rudder

48m
• Lecture 20 : Dihedral effect, Various contributions

44m
• Lecture 21 : Power effects, Roll control, Aileron

40m
• Lecture 22 : Example problems

51m

## Equations of Rigid Aircraft Six-Degree-of-Freedom Motion

• Lecture 23 : Derivation of Translational Motion Equations

43m
• Lecture 24 : Derivation of Angular Motion Equations

50m
• Lecture 25 : Description of various forces and moments

42m
• Lecture 26 : Nonlinearities and Associated Aircraft Behavior

52m

## Perturbed (Linear) Aircraft Model

• Lecture 27 : Small perturbation method, Linearization of equations?

45m
• Lecture 28 : Aerodynamic force and Moment Derivatives

50m
• Lecture 29 : Contribution of Aircraft components to Aerodynamic Derivatives

52m
• Lecture 30 : Linear Model and Aircraft Dynamics Modes

52m

## Longitudinal Dynamic Modes

• Lecture 31 : Short Period, Phugoid(Lanchester's formulation)

48m
• Lecture 32 : Short period mode approximation?

49m
• Lecture 33 : Flying and Handling Qualities, Cooper Harper Scale

48m

## Lateral-directional Dynamic Modes

• Lecture 34 : Pure rolling motion, Pure yawing motion,Spiral approximation

50m
• Lecture 35 : Spiral, Roll, Dutch roll Mode approximations

48m
• Lecture 36 : Lateral directional Flying Qualities, Routh's Stability criterion

45m
• Lecture 37 : Stability in Steady Roll Maneuver

49m

## Aircraft Response to External Inputs

• Lecture 38 : Wind Effect on Aircraft Pure Plunging Motion

47m
• Lecture 39 : Wind Profiles, Longitudinal Mode Response to Wind Shear

43m

## Introduction to Aircraft Control Systems

• Lecture 40 : Stability control/Augmentation

44m
• Lecture 41 : Autopilots, Automatic Landing System?

42m

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