Flight dynamics 2, stability

Flight dynamics - 2 ( stability ) , nptel iit, NIT videos

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Created by NPTL n Last updated Wed, 07-Oct-2020 English


Flight dynamics 2, stability free videos and free material uploaded by Indian Institute of Technology, chennai (IIT chennai). This session contains about Flight dynamics 2, stability Updated syllabus , Lecture notes , videos , MCQ , Privious Question papers and Toppers Training Provided Training of this course. If Material not uploaded check another subject

Syllabus / What will i learn?


Curriculum for this course
39 Lessons 31:05:47 Hours
Modul- 1
3 Lessons
  • Earth Atmosphere,Aircraft components,Aircraft nomenclature 00:47:57
  • Basic aerodynamics 00:56:14
  • Contribution of Aircraft components to Aerodynamic Derivatives 00:52:23
  • Equilibrium and stability 00:51:56
  • Static vs dynamic stability 00:41:50
  • Criterion for stability,Wing contribution 00:42:00
  • Horizontal tail contribution 00:52:34
  • Wing plus tail contribution 00:49:30
  • Static margin and CG limits 00:45:51
  • Fuselage contribution 00:49:23
  • Powerplant contribution 00:48:02
  • Power effects on neutral point 00:47:30
  • Elevator 00:41:21
  • Stick free stability, Most fwd CG location 00:47:40
  • Longitudinal stick force per 'g', Ground effect 00:44:14
  • Control requirement, Pull-up maneuver, Maneuver point 00:50:43
  • Elevator per 'g' , Maneuver point 00:49:39
  • Example problems 00:49:56
  • Lateral-Directional Stability Derivatives, Fuselage/Vertical fin contribution 00:50:12
  • Roll stability, Wing sweep effect, Rudder 00:48:40
  • Dihedral effect, Various contributions 00:44:56
  • Power effects, Roll control, Aileron 00:40:09
  • Derivation of Translational Motion Equations 00:43:40
  • Derivation of Angular Motion Equations 00:50:57
  • Description of various forces and moments 00:42:40
  • Nonlinearities and Associated Aircraft Behavior 00:52:11
  • Small perturbation method, Linearization of equations 00:45:49
  • Aerodynamic force and Moment Derivatives 00:50:59
  • Linear Model and Aircraft Dynamics Modes 00:52:05
  • Short Period, Phugoid(Lanchester's formulation) 00:48:27
  • Short period mode approximation 00:49:36
  • Flying and Handling Qualities, Cooper Harper Scale 00:48:15
  • Pure rolling motion, Pure yawing motion,Spiral approximation 00:50:10
  • Spiral, Roll, Dutch roll Mode approximations 00:48:54
  • Lateral directional Flying Qualities, Routh's Stability criterion 00:45:06
  • Stability in Steady Roll Maneuver 00:49:26
  • Wind Effect on Aircraft Pure Plunging Motion 00:47:14
  • Wind Profiles, Longitudinal Mode Response to Wind Shear 00:43:06
  • Stability control/Augmentation 00:44:32
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