2. Benchmark solution#

2.1. Calculation method used for the reference solution#

To calculate the added coefficients:

we show [bib1] that the added mass and damping coefficients depend on the permanent potential of the fluid speeds \(\stackrel{ˉ}{\phi }\) as well as on two fluctuating potentials \({\phi }_{1}\) and \({\phi }_{2}\): these potentials can be written in the case of the rotational movement of the external cylinder around the pivot C [bib1]:

_images/Object_12.svg

However, the added modal coefficients projected onto this mode of rotation can be written as:

_images/Object_13.svg

either:

_images/Object_14.svg

For the system with an equivalent degree of freedom:

It is a mass-spring-shock absorber system representing the rotational movement of the cylinder around the downstream pivot \(C\).

_images/1000032C00000CEB000008450E8D38D607DC8481.svg
  • The inertia of the mechanical system subjected to the flow is written as:

where

_images/Object_16.svg

is the inertia of the pivoting external cylinder with respect to the axis \(\mathrm{Cx}\) (see figure below) in air.

We show [bib2] that this inertia is equal to:

_images/Object_17.svg

where

_images/Object_18.svg

is the mass of the cylinder:

_images/Object_19.svg

where

_images/Object_20.svg

is the thickness of the cylinder,

_images/Object_21.svg

its total length.

_images/Object_22.svg

is the density of the cylinder.

_images/10002806000024CB000009180AB86993A0037FC4.svg

thus

_images/Object_23.svg
  • the damping of the mechanical system subjected to the flow is written as:

where

_images/Object_25.svg

is the damping of the mechanical system in air. Usually,

_images/Object_26.svg

is equal to a few% of the critical damping of the system:

_images/Object_27.svg

.

where

_images/Object_28.svg

is the inertia of the air cylinder calculated above and

_images/Object_29.svg

spring stiffness at the pivot point

_images/Object_30.svg

. We take the reduced depreciation

_images/Object_31.svg

equal to 1%.

Thus, the total damping of the system under flow is written as:

_images/Object_32.svg
  • the stiffness of the mechanical system subjected to flow is written as:

where

_images/Object_34.svg

is the stiffness of the spring in air.

_images/Object_35.svg

is the stiffness added by the flow. We show [bib1] that it is zero in this rotation mode.

_images/Object_36.svg

Thus the total rigidity of the system is independent of the flow speed.

_images/Object_37.svg
  • We then calculate the complex modes of this mechanical system under flow (damped free vibrations):

_images/Object_38.svg

The complex natural frequencies of this system are written as [bib3]:

_images/Object_39.svg

with

_images/Object_40.svg _images/Object_41.svg

: reduced system damping

_images/Object_42.svg

: natural pulsation.

  • Digital applications:

Three calculations of added damping were made corresponding to three flow velocities that cause three vibratory behaviors of the structure:

Speed to \(4m/s\)

Speed to \(4.24m/s\)

Speed to \(6m/s\)

The values of the mechanical system are:

_images/Object_43.svg

The added weight and damping provided by the flow are equal to:

_images/Object_44.svg

(independent of the flow speed value)

Depending on the fluid entry speed, we have:

_images/Object_45.svg

The amortization of the fluid/structure system is written as:

  • to

The flow does not amplify the vibrations. The internal structural damping is significant enough to dissipate the energy provided by the flow to the structure. The system is still depreciated.

  • to

The depreciation of the system is cancelled out.

  • to

The damping of the system at this last speed is negative: the system then enters floating instability.

The corresponding reduced amortization is written as:

_images/Object_49.svg

The natural pulsation remains unchanged:

_images/Object_50.svg

.

2.2. Benchmark results#

Analytical result.

2.3. Bibliographical references#

  1. ROUSSEAU G., LUU H.T.: Mass, damping and stiffness added for a vibrating structure placed in a potential flow - Bibliography and implementation in the*Code_Aster* - HP-61/95/064

  2. BLEVINS R.D: Formulas for natural frequency and mode shape. Ed. Krieger 1984

  3. SELIGMANN D, MICHEL R: Solving Algorithms for the Quadratic Problem [R5.01.02], Aster Reference Manual.