FLOPS based geometry modified#864
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jkirk5 merged 21 commits intoOpenMDAO:mainfrom Sep 12, 2025
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xjjiang
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jkirk5
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Sep 11, 2025
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Single question to double check a variable rename, but otherwise good to go!
Kenneth-T-Moore
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Sep 12, 2025
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Summary
In FLOPS based geometry:
CharacteristicLengthscomponent toWingCharacteristicLengthandOtherCharacteristicLength;_Fuselagecomponent to_Fuselageand_FuselageRatios.The purpose is to reuse the code as much as possible when BWB computation is added.
In FLOPS based geometry, there is no fuselage layout computation. If fuselage length or passenger compartment length is not given, it has to be computed using GASP based geometry. Now, there are two fuselage layout computations:
SimpleCabinLayoutandDetailedCabinLayout.SimpleCabinLayoutallows users to compute compartment length when fuselage length is given. If both compartment length and fuselage length are not given, they can be computed usingDetailedCabinLayout.There is no BWB component added yet.
Related Issues
Backwards incompatibilities
None
New Dependencies
None