Passive control of fluid-structure instabilities by means of - - PowerPoint PPT Presentation
Passive control of fluid-structure instabilities by means of - - PowerPoint PPT Presentation
Passive control of fluid-structure instabilities by means of piezo-shunts Marco CARINI, Jean-Lou PFISTER & Olivier MARQUET AEROFLEX project Piezo-electricity : a wide range of applications Piezo-electricity : Electric response of certain
Piezo-electricity : a wide range of applications
Piezo-electricity : Electric response of certain mate- rials to a mechanical stress due to their microscopic structure Sensing & Actuation from everyday life . . . . . . to the Aerospace Research Our Goal : using piezos to control fluid-structure instabilities
Carini, Pfister & Marquet 2 / 12 31 January 2017
2D Model problem
Fluid region Solid region Rigid cylinder + elastic plate + piezo patches. Re = U∞D/ν = 80, density ratio mρ = 50 and bending stiffness K = 0.3. Electro-mechanical coupling only acting for bending modes (transverse effect +
- pposite poiling direction).
Carini, Pfister & Marquet 3 / 12 31 January 2017
Modelling framework
Arbitrary Lagrangian Eulerian approach Lagrangian for the solid. Eulerian description for the fluid.
- Eqs. in the underformed configuration
Fully coupled nonlinear fluid-electro-mechanical system in compact form B ∂q ∂t = R(q). Linearization around a fixed equilibrium solution qB, i.e. R(qB) = 0, with q(x, t) = ˆ q(x)eλt λBˆ q = ∂R(q) ∂q
- qB
ˆ q, which is a Generalised Eigenvalue Problem, for λ = σ + ıω ∈ C :
Carini, Pfister & Marquet 4 / 12 31 January 2017
Base flow & Leading (unstable) modes
Base flow No Piezos Piezos
Carini, Pfister & Marquet 5 / 12 31 January 2017
Global spectrum
Without vs With Piezos
- 0.25
- 0.2
- 0.15
- 0.1
- 0.05
0.05 0.5 0.75 1 1.25 1.5
σ ω
Added electrical stiffness effect
Carini, Pfister & Marquet 6 / 12 31 January 2017
Connecting a R-shunt circuit
1st order electr. dynamics dQe dt + 1 RCp Qe = 0, τe = RCp is the characteristic electrical time. Energy dissipation by Joule’s effect, Pe = CpV 2
e /τe.
For τe → 0, electro-mechanical coupling becomes negligible (short-circuit). For τe → ∞, electro-mechanical coupling becomes maximal (open-circuit).
Carini, Pfister & Marquet 7 / 12 31 January 2017
Varying the electrical resistance
Leading eigenvalue
−6 −4 −2 1 2 3 −0.06 −0.03 0.03 0.06
σ log10 τe
−6 −4 −2 1 2 3 0.7 0.8 0.9 1 1.1
ω log10 τe
Carini, Pfister & Marquet 8 / 12 31 January 2017
Varying the electrical resistance (continued)
Increasing τe
- 0.2
- 0.15
- 0.1
- 0.05
0.05 0.6 0.8 1 1.2 σ ω
Carini, Pfister & Marquet 9 / 12 31 January 2017
System energy analysis
Leading mode
−6 −4 −2 1 2 3 0.4 0.8 1.2
Es% log10 τe
−6 −4 −2 1 2 3 4 8 12
Pe% log10 τe
×10−4
Carini, Pfister & Marquet 10 / 12 31 January 2017
Conclusions
A conjecture on two possible distinct stabilization mechanisms : Frequency desynchronization by means of the added electric stiffness (original flutter mode). Electrical damping through Joule effect (new selected flutter mode).
Carini, Pfister & Marquet 11 / 12 31 January 2017