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Aircraft Structural Dynamics

Dr. Anup Ghosh

3 followers

Aircraft Structural Dynamics

864 Learners

Aircraft Structural Dynamics

Validity Unlimited Aircraft Structural Dynamics All Level Aircraft Structural Dynamics English

0.0 (0)
Free

About This Course

An evaluation of aerodynamic and structural models is carried out for their application to flight dynamics of low-speed An evaluation of aerodynamic and structural models is carried out for their application to flight dynamics of low-speed aircraft with very-flexible high-aspect-ratio wings. The structural dynamic approaches include displacement-based, strain-based, and intrinsic (first-order) geometrically-nonlinear composite beam models, while thin-strip and vortexlattice methods are considered for the unsteady aerodynamics. We first show that all different beam finite-element models (previously derived in the literature from different assumptions) can be consistently obtained from a single set of equations.

  • Aircraft Structural Dynamics Total 16 Modules
  • Aircraft Structural Dynamics 43 Pdfs
  • Aircraft Structural Dynamics Downloadable on mobile
  • Aircraft Structural Dynamics Published on 18 June, 2019

Course Curriculum

Aerospace Structural Dynamics

Aircraft Structural Dynamics
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    Aerospace Structural Dynamics

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OSCILLATORY MOTION

Aircraft Structural Dynamics
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    OSCILLATORY MOTION

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    Oscillatory Motion (Contd.)

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Free vibration of Undamped Single Degree of Freedom System (SDOF)

Aircraft Structural Dynamics
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    Free vibration of Undamped Single Degree of Freedom System (SDOF)1

    5 pages <?php echo $alt; ?>

Transient Loading

Aircraft Structural Dynamics
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    Transient Loading1

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    Response of single dergree freedom with general type loading function (Forcing) Duhamals Integral, Convolution/Superposition Integral2

    4 pages <?php echo $alt; ?>
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    Laplace Transformation3

    3 pages <?php echo $alt; ?>

Numerical solution of a dynamic system

Aircraft Structural Dynamics
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    Numerical solution of a dynamic system

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    The Newmark Method

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System with two DOF

Aircraft Structural Dynamics
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    System with two DOF1

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    Numerical solution of a dynamic system2

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    Beat Phenomenon3

    5 pages <?php echo $alt; ?>
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    Co-ordinate Coupling4

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Response of 2DOF System to Harmonic Excitation

Aircraft Structural Dynamics
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    Response of 2DOF System to Harmonic Excitation

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    Vibration Absorber

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Steps of Modal Analysis

Aircraft Structural Dynamics
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    Steps of Modal Analysis

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    Steps of Modal Analysis (Contd.)

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    Steps of Modal Analysis (Contd.)

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    With viscous damping (under damped)

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Distributed Parameter Systems or Continuous Systems

Aircraft Structural Dynamics
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    Distributed Parameter Systems or Continuous Systems

    5 pages <?php echo $alt; ?>
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    Vibration of Bars or rods

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    Vibration of Bars or rods (Contd.)

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    Vibration of Bars or rods (Contd.)

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    Vibration of Bars or rods (Contd.)

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    Vibration of Bars or rods (Contd.)

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Approximate Methods

Aircraft Structural Dynamics
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    Approximate Methods

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    Rayleigh Ritz Method

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    Galerkins Method

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    Galerkins Method (Contd.)

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Derivation of the element stiffness matrix for a bar

Aircraft Structural Dynamics
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    Derivation of the element stiffness matrix for a bar

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    Derivation of the element stiffness matrix for a bar (Contd.)

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    Derivation of the element stiffness matrix for a bar (Contd.)

    6 pages <?php echo $alt; ?>
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    Derivation of the element stiffness matrix for a bar (Contd.)

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Damped Single-degree of Freedom System Free Vibration of Damped 2nd OrderSystem 3

Aircraft Structural Dynamics
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    Damped Single-degree of Freedom System Free Vibration of Damped 2nd OrderSystem

    5 pages <?php echo $alt; ?>
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    Damped Single-degree of Freedom System Free Vibration of Damped System(Contd.)2

    6 pages <?php echo $alt; ?>
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    Damped Single-degree of Freedom System Free Vibration of Damped System (Contd.)

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Characteristic of Harmonic Motion4

Aircraft Structural Dynamics
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    Characteristic of Harmonic Motion5

    7 pages <?php echo $alt; ?>

Response Due to Harmonic Excitation Forces6

Aircraft Structural Dynamics
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    Response Due to Harmonic Excitation Forces7

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    Response Due to Harmonic Excitation Forces (Contd.)8

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    Frequency response function9

    6 pages <?php echo $alt; ?>
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    Rotating Unbalance 10

    5 pages <?php echo $alt; ?>

Support Motion 11

Aircraft Structural Dynamics
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    Support Motion1

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Energy dissipated by damping1

Aircraft Structural Dynamics
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    Energy dissipated by damping2

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