4. B modeling#

4.1. Characteristics of modeling#

_images/100002B400001688000006836B505E07D12DEE4F.svg

The beam consists of a single mesh.

The modeling used for the beam is that of Euler-Bernoulli (POU_D_E).

The \(A\) end is embedded:

4.2. Characteristics of the mesh#

Number of knots: 2

Number of meshes and types: 1 mesh of type SEG 2

The characteristic points of the mesh are as follows:

4.3. Quantities tested (real/imaginary shape)#

Problem 1: traction (real distributed effort: zero imaginary part)

Point/Size

Reference value

Reference type

Precision (%)

displacement

B

DX

(5.318 10—5, 0. )

“ANALYTIQUE”

0.05

speed

B

DX

(0., 3.341 10—3)

“ANALYTIQUE”

0.05

acceleration

B

DX

(—2.099 10—1, 0. )

“ANALYTIQUE”

0.05

generalized effort

B

N

N

(3000., 0. )

“ANALYTIQUE”

0.05

Problem 2: traction (complex distributed effort: zero real part)

Point/Size

Reference value

Reference type

Precision (%)

displacement

B

DX

(0., 5.318 10—5)

“ANALYTIQUE”

0.05

speed

B

DX

(-3.341 10—3, 0. )

“ANALYTIQUE”

0.05

acceleration

B

DX

(0., —2.099 10—1)

“ANALYTIQUE”

0.05

generalized effort

B

N

N

(0., 3000. )

“ANALYTIQUE”

0.05

Problem 3: traction + damping (real distributed effort: zero imaginary part)

Point/Size

Reference value

Reference type

Precision (%)

displacement

B

DX

(5.296 10—5, —3.363 10—6)

“ANALYTIQUE”

DX

0.05

speed

B

DX

(2.113 10—4, 3.327 10—3)

“ANALYTIQUE”

0.05

acceleration

B

DX

(—2.091 10—1, 1.327 10—2)

“ANALYTIQUE”

0.05

generalized effort

B

N

N

(2.9879 103, —1.897 102)

“ANALYTIQUE”

0.05

Problem 4: flexure + damping (complex distributed force: zero real part)

Point/Size

Reference value

Reference type

Precision (%)

displacement

B

DX

(3.363 10—3, 5.296 10—5)

“ANALYTIQUE”

0.05

speed

B

DX

(-3.327 10—3, 2.113 10—4)

“ANALYTIQUE”

0.05

acceleration

B

DX

(-1.327 10—2, -2.091 10—1)

“ANALYTIQUE”

DX

0.05

generalized effort

B

N

N

(1.897 102, 2.9879 103)

“ANALYTIQUE”

0.05

When the distributed force is applied as an imaginary part of the load, the reference solution is obtained from that of modeling A by exchanging the real part and the imaginary part and by changing the sign of the new real parts.