Abstract
The growing interest to examine the hydroelastic dynamics and stabilities of lightweight and flexible materials requires robust and accurate fluid–structure interaction (FSI) models. Classically, partitioned fluid and structure solvers are easier to implement compared to monolithic methods; however, partitioned FSI models are vulnerable to numerical (“virtual added mass”) instabilities for cases when the solid to fluid density ratio is low and if the flow is incompressible. As a partitioned method, the loosely hybrid coupled (LHC) method, which was introduced and validated in Young et al. (Acta Mech. Sin. 28:1030–1041, 2012), has been successfully used to efficiently and stably model lightweight and flexible structures. The LHC method achieves its numerical stability by, in addition to the viscous fluid forces, embedding potential flow approximations of the fluid induced forces to transform the partitioned FSI model into a semi-implicit scheme. The objective of this work is to derive and validate the numerical stability boundary of the LHC. The results show that the stability boundary of the LHC is much wider than traditional loosely coupled methods for a variety of numerical integration schemes. The results also show that inclusion of an estimate of the fluid inertial forces is the most critical to ensure the numerical stability when solving for fluid–structure interaction problems involving cases with a solid to fluid-added mass ratio less than one.
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Notes
Note that the elastic axis can be pushed to the upstream of the center of pressure by either applying sweep (or skew) or by manipulating the mass and/or stiffness distribution by using non-homogenous, non-uniform, or anisotropic wings/foils.
Abbreviations
- \(A_\mathrm{c}^\mathrm{M} \) :
-
Nondimensional \(C_\mathrm{f}^\mathrm{M} \, (={C_\mathrm{f}^\mathrm{M} }/{\rho _\mathrm{f} Ub^{3}})\)
- \(A_\mathrm{k}^\mathrm{M} \) :
-
Nondimensional \(K_\mathrm{f}^\mathrm{M} \, (={K_\mathrm{f}^\mathrm{M} }/{\rho _\mathrm{f} U^{2}b^{2}})\)
- \(A_\mathrm{m}^\mathrm{M} \) :
-
Nondimensional \(M_\mathrm{f}^\mathrm{M} \,(={M_\mathrm{f}^\mathrm{M} }/{\rho _\mathrm{f} b^{4}})\)
- \(A_\mathrm{c}^\mathrm{P} \) :
-
Nondimensional \(C_\mathrm{f}^\mathrm{P} \,(={C_\mathrm{f}^\mathrm{P} }/{\rho _\mathrm{f} Ub^{3}})\)
- \(A_\mathrm{k}^\mathrm{P} \) :
-
Nondimensional \(K_\mathrm{f}^\mathrm{P} \,(={K_\mathrm{f}^\mathrm{P} }/{\rho _\mathrm{f} U^{2}b^{2}})\)
- \(A_\mathrm{m}^\mathrm{P} \) :
-
Nondimensional \(M_\mathrm{f}^\mathrm{P} \,(={M_\mathrm{f}^\mathrm{P} }/{\rho _\mathrm{f} b^{4}})\)
- ba :
-
Distance to E.A. from the foil’s mid-chord location
- b :
-
Foil’s half chord length
- \(\mathbf{C}\) :
-
Foil’s nondimensional radius of gyration \((={I_\theta }/{\rho _\mathrm{s} b^{4}})\)
- C.G.:
-
Foil’s center of gravity
- \(\tilde{C}_\mathrm{e}\) :
-
Part of the total fluid and solid damping treated explicitly (Eq. (12))
- \(C_\mathrm{f}^\mathrm{M}\) :
-
Empirically estimated fluid–induced torsion damping from experiments and viscous simulations
- \(C_\mathrm{f}^\mathrm{P}\) :
-
Potential-flow estimation of the fluid–induced torsion damping
- \(\tilde{C}_\mathrm{i}\) :
-
Part of the total fluid and solid damping treated implicitly (Eq. (12))
- \(C_\theta \) :
-
Foil’s torsional damping value per unit span
- c :
-
Foil’s chord length
- DOF:
-
Degree of freedom
- E.A.:
-
Foil’s elastic axis
- FC:
-
Fully-coupled
- FSI:
-
Fluid–structure interaction
- \(I_\theta \) :
-
Foil’s mass moment of inertia per unit span
- \(\tilde{K}_\mathrm{e}\) :
-
Part of the total fluid and solid damping treated explicitly (Eq. (12))
- \(K_\mathrm{f}^\mathrm{M}\) :
-
Empirically estimated fluid–induced torsion stiffness from experiments and viscous simulations
- \(K_\mathrm{f}^\mathrm{P}\) :
-
Potential-flow estimation of the fluid–induced torsion stiffness
- \(\tilde{K}_\mathrm{i}\) :
-
Part of the total fluid and solid damping treated implicitly (Eq. (12))
- \(K_\theta \) :
-
Foil’s torsional stiffness per unit span
- k :
-
Reduced frequency \((={\omega b}/U)\)
- LC:
-
Loosely coupled
- LHC:
-
Loosely hybrid coupled
- \(\tilde{M}_\mathrm{e} \) :
-
Part of the total fluid and solid mass treated explicitly (Eq. (12))
- \(M_\mathrm{f}^\mathrm{M} \) :
-
Empirically estimated fluid-added moment of inertia from experiments or viscous simulations
- \(M_\mathrm{f}^\mathrm{P} \) :
-
Potential-flow estimation of the fluid-added moment of inertia
- \(M_{\mathrm{fluid}}\) :
-
Fluid–induced moment per unit span
- \(M_{\mathrm{fluid}}^\mathrm{E} \) :
-
Estimated fluid–induced moment per unit span
- \(M_{\mathrm{fluid}}^\mathrm{M}\) :
-
Empirically estimated fluid–induced moment on the foil per unit span from experiments or viscous simulations
- \(M_{\mathrm{fluid}}^\mathrm{P} \) :
-
Potential-flow estimation of the fluid–induced moment per unit span
- \(\tilde{M}_\mathrm{i} \) :
-
Part of the total fluid and solid mass treated implicitly (Eq. (12))
- n :
-
Discrete time-level \((t=n\Delta t)\)
- Re :
-
Reynolds number \((={Uc}/{\upsilon _\mathrm{f} })\)
- s :
-
Foil’s span length
- t :
-
Time
- \(\bar{{t}}\) :
-
Nondimensional time \((={tU}/b)\)
- U :
-
Inflow speed
- \(\bar{{U}}\) :
-
Reduced speed \((=U/b\omega _\theta )\)
- \(x_\theta \) :
-
Distance to the C.G. from E.A. positive towards the foil trailing edge
- \(\alpha \) :
-
Fraction of the fluid-added mass used for \(A_\mathrm{m}^\mathrm{P} \)–\(A_\mathrm{m}^\mathrm{M} \)
- \(\Delta t\) :
-
Time-step size
- \(\Delta \bar{{t}}\) :
-
Nondimensional time-step size
- \(\theta \) :
-
Foil’s twist angle at its E.A.
- \(\lambda \) :
-
Growth factor (in time) of \(\theta \, (\theta _{n+1} =\lambda \theta _n )\)
- \(\mu \) :
-
Solid to fluid density ratio \((={\rho _\mathrm{s} }/{\rho _\mathrm{f} })\)
- \(\upsilon _\mathrm{f} \) :
-
Fluid’s kinematic viscosity
- \(\xi _\theta \) :
-
Foil’s damping coefficient in air \((={C_\theta }/{2I_\theta \omega _\theta })\)
- \(\rho _\mathrm{f} \) :
-
Fluid’s density
- \(\rho _\mathrm{s} \) :
-
Foil’s density
- \(\phi \) :
-
Theodorsen’s function (Eq. (36))
- \(\omega \) :
-
Foil’s primary vibration frequency
- \(\omega _\mathrm{n} \) :
-
Foil’s twisting natural frequency in water
- \(\omega _\theta \) :
-
Foil’s twisting natural frequency in air
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Acknowledgements
The authors would like to acknowledge the financial support received from the Office of Naval Research (ONR) (Grants N00014-11-1-0833 and N00014-13-1-0383) managed by Ms. Kelly Cooper and Dr. Ki-Han Kim, respectively.
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Appendix
Appendix
1.1 A1 Time-discretization of Eq. (12) for Scheme B shown in Eq. (14)
Scheme B uses the Crank–Nicholson method to approximate \(\dot{\bar{{\theta }}}\) and \(\ddot{\bar{{\theta }}}\) as
Re-arranging Eqs. (A1) and (A2) yield
and, hence,
Using Eqs. (A3) and (A5) in Eq. (12), in addition to Eqs. (A3) and (A5) themselves result in the linear system shown in Eq. (14), which could be solved in terms of \(\theta _{n+1} \), \(\dot{\bar{{\theta }}}_{n+1} \), and \(\ddot{\bar{{\theta }}}_{n+1} \).
1.2 A2 Time-discretization of Eq. (12) for Scheme C shown in Eq. (15)
Scheme C is constructed by converting the second-order differential equation (Eq. (12)) into two first-order differential equations for (\(\theta \), \(\dot{\bar{{\theta }}})\) as
Scheme C discretizes Eqs. (A6) and (A7) as
Equation (A8) is the Crank–Nicholson discretization of Eq. (A6). To get Eq. (A9), Eq. (A7) has been discretized by treating its left-hand side of Eq. (A7) implicitly, and right-hand side explicitly. The combined linear system of Eqs. (A8) and (A9) is given as Eq. (15).
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Akcabay, D.T., Xiao, J. & Young, Y.L. Numerical stabilities of loosely coupled methods for robust modeling of lightweight and flexible structures in incompressible and viscous flows. Acta Mech. Sin. 33, 709–724 (2017). https://doi.org/10.1007/s10409-017-0696-1
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DOI: https://doi.org/10.1007/s10409-017-0696-1