54. Wing with boundary pressure

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

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 55 Test results

test

case

scalar

expected

output

delta

tolerance

status

test_path

0054

LC1_pressure_1_0_0

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

-9.9998E+02

-1.0015E+03

0.2%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC1_pressure_1_0_0

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

+0.0000E+00

+8.3617E-08

-0.00

0.10

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC1_pressure_1_0_0

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

+0.0000E+00

-1.9867E-07

0.00

0.10

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC1_pressure_1_0_0

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

+0.0000E+00

-2.0389E-07

0.00

0.10

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC1_pressure_1_0_0

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

-9.0408E+00

-9.0134E+00

-0.3%

0.03

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC1_pressure_1_0_0

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

+8.7499E+02

+8.7635E+02

0.2%

0.03

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC2_pressure_0_1_0

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

+0.0000E+00

-6.9858E-08

0.00

0.10

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC2_pressure_0_1_0

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

-9.9998E+02

-1.0015E+03

0.2%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC2_pressure_0_1_0

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

+0.0000E+00

-4.9741E-06

0.00

0.10

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC2_pressure_0_1_0

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

+9.0408E+00

+9.0134E+00

-0.3%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC2_pressure_0_1_0

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

+0.0000E+00

+2.9398E-09

-0.00

0.10

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC2_pressure_0_1_0

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

-2.4284E+00

-2.3573E+00

-2.9%

0.03

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC3_pressure_0_0_1

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

+0.0000E+00

-1.8757E-06

0.00

0.10

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC3_pressure_0_0_1

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

+0.0000E+00

-8.2078E-06

0.00

0.10

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC3_pressure_0_0_1

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

-9.9998E+02

-1.0015E+03

0.2%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC3_pressure_0_0_1

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

-8.7499E+02

-8.7635E+02

0.2%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC3_pressure_0_0_1

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

+2.4284E+00

+2.3573E+00

-2.9%

0.03

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC3_pressure_0_0_1

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

+0.0000E+00

+2.6515E-06

-0.00

0.10

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC4_pressure_1_0_1

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

-9.9998E+02

-1.0015E+03

0.2%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC4_pressure_1_0_1

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

+0.0000E+00

-8.1242E-06

0.00

0.10

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC4_pressure_1_0_1

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

-9.9998E+02

-1.0015E+03

0.2%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC4_pressure_1_0_1

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

-8.7498E+02

-8.7635E+02

0.2%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC4_pressure_1_0_1

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

-6.6124E+00

-6.6561E+00

0.7%

0.03

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC4_pressure_1_0_1

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

+8.7498E+02

+8.7635E+02

0.2%

0.03

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC5_pressure_1_1_1

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

-9.9998E+02

-1.0015E+03

0.2%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC5_pressure_1_1_1

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

-9.9998E+02

-1.0015E+03

0.2%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC5_pressure_1_1_1

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

-9.9998E+02

-1.0015E+03

0.2%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC5_pressure_1_1_1

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

-8.6594E+02

-8.6733E+02

0.2%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC5_pressure_1_1_1

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

-6.6124E+00

-6.6561E+00

0.7%

0.03

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC5_pressure_1_1_1

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

+8.7256E+02

+8.7399E+02

0.2%

0.03

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC6_pressure_1+1+1

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

-9.9998E+02

-1.0015E+03

0.2%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC6_pressure_1+1+1

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

-9.9998E+02

-1.0015E+03

0.2%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC6_pressure_1+1+1

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

-9.9998E+02

-1.0015E+03

0.2%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC6_pressure_1+1+1

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

-8.6595E+02

-8.6733E+02

0.2%

0.01

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC6_pressure_1+1+1

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

-6.6124E+00

-6.6561E+00

0.7%

0.03

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure

0054

LC6_pressure_1+1+1

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

+8.7256E+02

+8.7399E+02

0.2%

0.03

✓ pass

0054_geometry-0020_aligned-wing-boundary-pressure