Course10110604241 lectures
Flight Dynamics II (Stability)
Dr. Nandan Kumar Sinha · IIT Madras
Lectures
Introduction to the course
- Lecture 1 : Earth Atmosphere, Aircraft components, Aircraft nomenclature
- Lecture 2 : Basic aerodynamics
Equilibrium and stability
Longitudinal static stick fixed stability
- Lecture 5 : Criterion for stability, Wing contribution
- Lecture 6 : Horizontal tail contribution
- Lecture 7 : Wing plus tail contribution
Longitudinal stability and neutral point
- Lecture 8 : Static margin and CG limits
- Lecture 9 : Fuselage contribution
- Lecture 10 : Powerplant contribution
- Lecture 11 : Power effects on neutral point
Longitudinal control
- Lecture 12 : Elevator
- Lecture 13 : Stick free stability, Most fwd CG location
- Lecture 14 : Longitudinal stick force per 'g', Ground effect
Longitudinal control and maneuverability
- Lecture 15 : Control requirement, Pull-up maneuver,Maneuver point
- Lecture 16 : Elevator per 'g' , Maneuver point
- Lecture 17 : Example problems
Lateral directional static stability and control
- Lecture 18 : Lateral-Directional Stability Derivatives, Fuselage/Vertical fin contribution
- Lecture 19 : Roll stability, Wing sweep effect, Rudder
- Lecture 20 : Dihedral effect, Various contributions
- Lecture 21 : Power effects, Roll control, Aileron
- Lecture 22 : Example problems
Equations of Rigid Aircraft Six-Degree-of-Freedom Motion
- Lecture 23 : Derivation of Translational Motion Equations
- Lecture 24 : Derivation of Angular Motion Equations
- Lecture 25 : Description of various forces and moments
- Lecture 26 : Nonlinearities and Associated Aircraft Behavior
Perturbed (Linear) Aircraft Model
- Lecture 27 : Small perturbation method, Linearization of equations
- Lecture 28 : Aerodynamic force and Moment Derivatives
- Lecture 29 : Contribution of Aircraft components to Aerodynamic Derivatives
- Lecture 30 : Linear Model and Aircraft Dynamics Modes
Longitudinal Dynamic Modes
- Lecture 31 : Short Period, Phugoid(Lanchester's formulation)
- Lecture 32 : Short period mode approximation
- Lecture 33 : Flying and Handling Qualities, Cooper Harper Scale
Lateral-directional Dynamic Modes
- Lecture 34 : Pure rolling motion, Pure yawing motion,Spiral approximation
- Lecture 35 : Spiral, Roll, Dutch roll Mode approximations
- Lecture 36 : Lateral directional Flying Qualities, Routh's Stability criterion
- Lecture 37 : Stability in Steady Roll Maneuver
Aircraft Response to External Inputs
- Lecture 38 : Wind Effect on Aircraft Pure Plunging Motion
- Lecture 39 : Wind Profiles, Longitudinal Mode Response to Wind Shear
Introduction to Aircraft Control Systems
Syllabus and materials
At NPTEL, as the course publishes them.
Credits and licence
- Institution
- IIT Madras
- Department
- Aerospace Engineering
- Teacher
- Dr. Nandan Kumar Sinha
- Level
- Undergraduate
- Language
- English
- Subjects
- Engineering
- Source
- NPTEL
- Licence
- CC BY-NC-SA, as NPTEL states it. Non-commercial use only. NPTEL's terms
- Attribution
- NPTEL states: "Distributed under Creative Commons Attribution-ShareAlike / CC BY - NC - SA", beside a BY-NC-SA badge.
- Who can watch
- NPTEL gives no rating. Invisible Network shows it to Tweens profiles and older, judged from what the source says about it. How courses are placed
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