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Set mass default#640

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xjjiang wants to merge 28 commits intoOpenMDAO:mainOpenMDAO/Aviary:mainfrom xjjiang:set_mass_defaultxjjiang/om-Aviary:set_mass_defaultCopy head branch name to clipboard

+475-603

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Commits on Jan 6, 2025

• work in progress.

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• work in progress.

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Commits on Jan 7, 2025

• work in progress.

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• work in progress

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• minor change

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• Merge branch 'main' into set_mass_default

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Commits on Jan 8, 2025

• set Aircraft.Engine.MASS_SCALER = 0 instead of 1 because that is in the unit test.

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• minor update

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• removed new addition of Aircraft.Strut.MASS_COEFFICIENT setting because it caused compilation error.

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• added missing variable Aircraft.Engine.ADDITIONAL_MASS_FRACTION = 0.14.

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• keep shape=None in add_aviary_output()

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• add Aircraft.Wing.SLAT_SPAN_RATIO and Aircraft.Wing.SLAT_CHORD_RATIO to PreMissionTestCase

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• autopep8

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• autopep8

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Commits on Jan 9, 2025

• set Aircraft.Engine.ADDITIONAL_MASS_FRACTIO = val=np.full(num_engine_type, 0.14)

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• Merge branch 'OpenMDAO:main' into set_mass_default

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• minor update

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Commits on Jan 10, 2025

• add aircraft:wing:slat_span_ratio

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• remove temperary comments

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• remove a few vals

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• remove val from Aircraft.Fuel.DENSITY but keep the units because there are two different units in four components

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• set ASPECT_RATIO to 0.0

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Commits on Jan 13, 2025

• set Aircraft.HorizontalTail.TAPER_RATIO = 0.0

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Commits on Jan 14, 2025

• Merge branch 'OpenMDAO:main' into set_mass_default

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Commits on Jan 17, 2025

• Merge branch 'main' into set_mass_default

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Commits on Jan 18, 2025

• Merge branch 'main' into set_mass_default

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Commits on Jan 22, 2025

• Merge branch 'OpenMDAO:main' into set_mass_default

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Commits on Jan 25, 2025

• Merge branch 'OpenMDAO:main' into set_mass_default

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