• Component

    École Nationale Supérieure d'Électrotechnique d'Électronique

Objectives

  • Know how to identify the mechanism causing a vibration problem of a structure placed in a flow.     
  • Knowing how to choose the acquisition and processing parameters to identify the modes of an aeroelastic system by spectral analysis.
Read more

Description

I. Physics of the interaction     

 

  • Examples and industrial context, classification by dimensional analysis, aerodynamic complements.     
  • Vortex-induced vibration, lock-in     
  • Stability analysis, damping and added stiffness (galloping, divergence)     
  • Aeroelastic transients, dynamic stall, hereditary damping    
  •  State formalism, modal analysis, antisymmetric stiffness coupling (flutter flexion-torsion of a wing).

 

II. Experimental identification    

 

  • Periodic estimation of Welch, statistical properties    
  •  Method of identification of fluidelastic coupling (direct or indirect)     
  • Filtering relations (Wiener-Lee), consistency function     
  • Practical application (TP) to spectral and correlation analysis "real time" of a flexible structure in a turbulent flow. Identification of a Movement Induced Vibration (MIV) coupling
Read more

Additional information