Flight Dynamics II (Stability) NPTEL
Online Free Online Course by
World Mentoring Academy
Online
/ Free Online Course
Details
Description: Airplane nomenclature and aerodynamics, Review of basics of rigid body dynamics, Concepts of static and dynamic stability, Need for stability in an airplane, Purpose of controls, Inherently and marginally stable airplanes,Longitudinal
and Lateral directional static stability.
Resources: OpenCourseware from NPTEL (India), Sheridan College, MIT, UC Berkeley, Stanford & many other of the World's finest University's
Language: English
Professors: Michael Williams
Units: 41
Lesson content
- 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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