Flight Dynamics II (Stability) - Study24x7
Social learning Network
Flight Dynamics II (Stability)
broucher Course Brochure
Flight Dynamics II (Stability)
by Dr Nandan Kumar Sinha

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. ......

0.0  (0 Ratings) 0 Learner
validy img Validity Unlimited
level All Level
level English
cover Img Preview not available
Program Fee
FREE
About This Course

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. ......

Course Curriculum
13 Sections | 41 Lecture | 32h 40min total length
Expand all sections
Flight Dynamics II (Stability)

Introduction to the course

| 01h 44min total length
  • <?php echo $alt; ?>

    Lecture 1 : Earth Atmosphere, Aircraft components, Aircraft nomenclature

    47m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 2 : Basic aerodynamics

    56m <?php echo $alt; ?>
Flight Dynamics II (Stability)

Equilibrium and stability

| 01h 33min total length
  • <?php echo $alt; ?>

    Lecture 3 : Equilibrium and stability

    51m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 4 : Static vs dynamic stability

    41m <?php echo $alt; ?>
Flight Dynamics II (Stability)

Longitudinal static stick fixed stability

| 02h 24min total length
  • <?php echo $alt; ?>

    Lecture 5 : Criterion for stability, Wing contribution

    42m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 6 : Horizontal tail contribution

    52m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 7 : Wing plus tail contribution

    49m <?php echo $alt; ?>
Flight Dynamics II (Stability)

Longitudinal stability and neutral point

| 03h 10min total length
  • <?php echo $alt; ?>

    Lecture 8 : Static margin and CG limits

    45m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 9 : Fuselage contribution

    49m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 10 : Powerplant contribution

    48m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 11 : Power effects on neutral point

    47m <?php echo $alt; ?>
Flight Dynamics II (Stability)

Longitudinal control

| 02h 13min total length
  • <?php echo $alt; ?>

    Lecture 12 : Elevator

    41m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 13 : Stick free stability, Most fwd CG location

    47m <?php echo $alt; ?>
  • <?php echo $alt; ?>

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

    44m <?php echo $alt; ?>
Flight Dynamics II (Stability)

Longitudinal control and maneuverability

| 02h 30min total length
  • <?php echo $alt; ?>

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

    50m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 16 : Elevator per 'g' , Maneuver point

    49m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 17 : Example problems

    49m <?php echo $alt; ?>
Flight Dynamics II (Stability)

Lateral directional static stability and control

| 03h 55min total length
  • <?php echo $alt; ?>

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

    50m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 19 : Roll stability, Wing sweep effect, Rudder

    48m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 20 : Dihedral effect, Various contributions

    44m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 21 : Power effects, Roll control, Aileron

    40m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 22 : Example problems

    51m <?php echo $alt; ?>
Flight Dynamics II (Stability)

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

| 03h 09min total length
  • <?php echo $alt; ?>

    Lecture 23 : Derivation of Translational Motion Equations

    43m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 24 : Derivation of Angular Motion Equations

    50m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 25 : Description of various forces and moments

    42m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 26 : Nonlinearities and Associated Aircraft Behavior

    52m <?php echo $alt; ?>
Flight Dynamics II (Stability)

Perturbed (Linear) Aircraft Model

| 03h 21min total length
  • <?php echo $alt; ?>

    Lecture 27 : Small perturbation method, Linearization of equations?

    45m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 28 : Aerodynamic force and Moment Derivatives

    50m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 29 : Contribution of Aircraft components to Aerodynamic Derivatives

    52m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 30 : Linear Model and Aircraft Dynamics Modes

    52m <?php echo $alt; ?>
Flight Dynamics II (Stability)

Longitudinal Dynamic Modes

| 02h 26min total length
  • <?php echo $alt; ?>

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

    48m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 32 : Short period mode approximation?

    49m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 33 : Flying and Handling Qualities, Cooper Harper Scale

    48m <?php echo $alt; ?>
Flight Dynamics II (Stability)

Lateral-directional Dynamic Modes

| 03h 13min total length
  • <?php echo $alt; ?>

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

    50m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 35 : Spiral, Roll, Dutch roll Mode approximations

    48m <?php echo $alt; ?>
  • <?php echo $alt; ?>

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

    45m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 37 : Stability in Steady Roll Maneuver

    49m <?php echo $alt; ?>
Flight Dynamics II (Stability)

Aircraft Response to External Inputs

| 01h 30min total length
  • <?php echo $alt; ?>

    Lecture 38 : Wind Effect on Aircraft Pure Plunging Motion

    47m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 39 : Wind Profiles, Longitudinal Mode Response to Wind Shear

    43m <?php echo $alt; ?>
Flight Dynamics II (Stability)

Introduction to Aircraft Control Systems

| 01h 27min total length
  • <?php echo $alt; ?>

    Lecture 40 : Stability control/Augmentation

    44m <?php echo $alt; ?>
  • <?php echo $alt; ?>

    Lecture 41 : Autopilots, Automatic Landing System?

    42m <?php echo $alt; ?>
show 10 more sections
More Courses by Dr Nandan Kumar Sinha

Space Technology

by Dr Nandan Kumar Sinha
5.0 (0)

2 Enrollments

Validity Unlimited

Free