60. Wing with a coupled beam and boundary pressure

This test covers boundary pressure loads applied to a wing model with a coupled beam.

Geometry and setup

This test uses geometry 20 wing aligned with y.

Load cases

  • LC1_pressure_1_0_0: Pressure vector applied at the end surface along x

  • LC2_pressure_0_1_0: Pressure vector applied at the end surface along y

  • LC3_pressure_0_0_1: Pressure vector applied at the end surface along z

  • LC4_pressure_1_0_1: Pressure vector applied at the end surface along (1,0,1)

  • LC5_pressure_1_1_1: Pressure vector applied at the end surface along (1,1,1)

  • LC6_pressure_1+1+1: Consecutive pressure vectors at the end surface along each of the cartesian directions

Test results

Table last updated on September 10, 2025 at 13:44 UTC

Version: 2025.09.10.1323_fcc273e8

Table 61 Test results

test

case

scalar

expected

output

delta

tolerance

status

test_path

0060

LC1_pressure_1_0_0

reaction_forces > solid.1 > surface_set > fix > RFx (N)

-9.9998E+02

-9.9919E+02

-0.1%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC1_pressure_1_0_0

reaction_forces > solid.1 > surface_set > fix > RFy (N)

+0.0000E+00

+8.3441E-08

-0.00

0.10

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC1_pressure_1_0_0

reaction_forces > solid.1 > surface_set > fix > RFz (N)

+0.0000E+00

-1.8943E-07

0.00

0.10

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC1_pressure_1_0_0

reaction_moments > solid.1 > surface_set > fix > RMx (Nm)

+0.0000E+00

-1.9766E-07

0.00

0.10

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC1_pressure_1_0_0

reaction_moments > solid.1 > surface_set > fix > RMy (Nm)

-9.0408E+00

-8.9923E+00

-0.5%

0.04

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC1_pressure_1_0_0

reaction_moments > solid.1 > surface_set > fix > RMz (Nm)

+8.7499E+02

+8.7429E+02

-0.1%

0.04

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC2_pressure_0_1_0

reaction_forces > solid.1 > surface_set > fix > RFx (N)

+0.0000E+00

-7.0330E-08

0.00

0.10

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC2_pressure_0_1_0

reaction_forces > solid.1 > surface_set > fix > RFy (N)

-9.9998E+02

-9.9919E+02

-0.1%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC2_pressure_0_1_0

reaction_forces > solid.1 > surface_set > fix > RFz (N)

+0.0000E+00

-4.9682E-06

0.00

0.10

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC2_pressure_0_1_0

reaction_moments > solid.1 > surface_set > fix > RMx (Nm)

+9.0408E+00

+8.9923E+00

-0.5%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC2_pressure_0_1_0

reaction_moments > solid.1 > surface_set > fix > RMy (Nm)

+0.0000E+00

+2.8863E-09

-0.00

0.10

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC2_pressure_0_1_0

reaction_moments > solid.1 > surface_set > fix > RMz (Nm)

-2.4284E+00

-2.3518E+00

-3.2%

0.04

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC3_pressure_0_0_1

reaction_forces > solid.1 > surface_set > fix > RFx (N)

+0.0000E+00

-1.7742E-06

0.00

0.10

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC3_pressure_0_0_1

reaction_forces > solid.1 > surface_set > fix > RFy (N)

+0.0000E+00

-7.8644E-06

0.00

0.10

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC3_pressure_0_0_1

reaction_forces > solid.1 > surface_set > fix > RFz (N)

-9.9998E+02

-9.9919E+02

-0.1%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC3_pressure_0_0_1

reaction_moments > solid.1 > surface_set > fix > RMx (Nm)

-8.7499E+02

-8.7429E+02

-0.1%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC3_pressure_0_0_1

reaction_moments > solid.1 > surface_set > fix > RMy (Nm)

+2.4284E+00

+2.3518E+00

-3.2%

0.04

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC3_pressure_0_0_1

reaction_moments > solid.1 > surface_set > fix > RMz (Nm)

+0.0000E+00

+2.5582E-06

-0.00

0.10

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC4_pressure_1_0_1

reaction_forces > solid.1 > surface_set > fix > RFx (N)

-9.9998E+02

-9.9919E+02

-0.1%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC4_pressure_1_0_1

reaction_forces > solid.1 > surface_set > fix > RFy (N)

+0.0000E+00

-7.7811E-06

0.00

0.10

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC4_pressure_1_0_1

reaction_forces > solid.1 > surface_set > fix > RFz (N)

-9.9998E+02

-9.9919E+02

-0.1%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC4_pressure_1_0_1

reaction_moments > solid.1 > surface_set > fix > RMx (Nm)

-8.7498E+02

-8.7429E+02

-0.1%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC4_pressure_1_0_1

reaction_moments > solid.1 > surface_set > fix > RMy (Nm)

-6.6124E+00

-6.6405E+00

0.4%

0.04

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC4_pressure_1_0_1

reaction_moments > solid.1 > surface_set > fix > RMz (Nm)

+8.7498E+02

+8.7429E+02

-0.1%

0.04

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC5_pressure_1_1_1

reaction_forces > solid.1 > surface_set > fix > RFx (N)

-9.9998E+02

-9.9919E+02

-0.1%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC5_pressure_1_1_1

reaction_forces > solid.1 > surface_set > fix > RFy (N)

-9.9998E+02

-9.9919E+02

-0.1%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC5_pressure_1_1_1

reaction_forces > solid.1 > surface_set > fix > RFz (N)

-9.9998E+02

-9.9919E+02

-0.1%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC5_pressure_1_1_1

reaction_moments > solid.1 > surface_set > fix > RMx (Nm)

-8.6594E+02

-8.6530E+02

-0.1%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC5_pressure_1_1_1

reaction_moments > solid.1 > surface_set > fix > RMy (Nm)

-6.6124E+00

-6.6405E+00

0.4%

0.04

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC5_pressure_1_1_1

reaction_moments > solid.1 > surface_set > fix > RMz (Nm)

+8.7256E+02

+8.7194E+02

-0.1%

0.04

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC6_pressure_1+1+1

reaction_forces > solid.1 > surface_set > fix > RFx (N)

-9.9998E+02

-9.9919E+02

-0.1%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC6_pressure_1+1+1

reaction_forces > solid.1 > surface_set > fix > RFy (N)

-9.9998E+02

-9.9919E+02

-0.1%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC6_pressure_1+1+1

reaction_forces > solid.1 > surface_set > fix > RFz (N)

-9.9998E+02

-9.9919E+02

-0.1%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC6_pressure_1+1+1

reaction_moments > solid.1 > surface_set > fix > RMx (Nm)

-8.6595E+02

-8.6530E+02

-0.1%

0.01

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC6_pressure_1+1+1

reaction_moments > solid.1 > surface_set > fix > RMy (Nm)

-6.6124E+00

-6.6405E+00

0.4%

0.04

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure

0060

LC6_pressure_1+1+1

reaction_moments > solid.1 > surface_set > fix > RMz (Nm)

+8.7256E+02

+8.7194E+02

-0.1%

0.04

✓ pass

0060_geometry-0020_coupled-aligned-wing-boundary-pressure