Aerospace - Flight Dynamics II (Stability) (English)

   Thursday, March 20, 2025   

Starting a new Lecture Notes Series on Aerospace - Flight Dynamics II (Stability)

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Aerospace - Flight Dynamics II (Stability) By Lecture Notes together!

Lecture 1: Mod-01 Lec-01 Earth Atmosphere,Aircraft components,Aircraft nomenclature

Lecture 2: Mod-01 Lec-02 Basic aerodynamics

Lecture 3: Mod-02 Lec-03 Equilibrium and stability

Lecture 4: Mod-02 Lec-04 Static vs dynamic stability

Lecture 5: Mod-03 Lec-05 Criterion for stability,Wing contribution

Lecture 6: Mod-03 Lec-06 Horizontal tail contribution

Lecture 7: Mod-03 Lec-07 Wing plus tail contribution

Lecture 8: Mod-04 Lec-08 Static margin and CG limits

Lecture 9: Mod-04 Lec-09 Fuselage contribution

Lecture 10: Mod-04 Lec-10 Powerplant contribution

Lecture 11: Mod-04 Lec-11 Power effects on neutral point

Lecture 12: Mod-05 Lec-12 Elevator

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

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

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

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

Lecture 17: Mod-06 Lec-17 Example problems

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

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

Lecture 20: Mod-07 Lec-20 Dihedral effect, Various contributions

Lecture 21: Mod-07 Lec-21 Power effects, Roll control, Aileron

Lecture 22: Mod-07 Lec-22 Example problems

Lecture 23: Mod-08 Lec-23 Derivation of Translational Motion Equations

Lecture 24: Mod-08 Lec-24 Derivation of Angular Motion Equations

Lecture 25: Mod-08 Lec-25 Description of various forces and momentsMod-08 Lec-25 Description of various forces and moments

Lecture 26: Mod-08 Lec-26 Nonlinearities and Associated Aircraft Behavior

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

Lecture 28: Mod-09 Lec-28 Aerodynamic force and Moment Derivatives

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

Lecture 30: Mod-09 Lec-30 Linear Model and Aircraft Dynamics Modes

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

Lecture 32: Mod-10 Lec-32 Short period mode approximation

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

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

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

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

Lecture 37: Mod-11 Lec-37 Stability in Steady Roll Maneuver

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

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

Lecture 40: Mod-13 Lec-40 Stability control/Augmentation

Lecture 41: Mod-13 Lec-41 Autopilots, Automatic Landing System