Dear John and colleagues,
I have two questions for Thursday's meeting, I plan to attend but I prefer to post them already.
- The challenge paper mentions the fuselage backup structure as part of the path of the aerodynamic loads. However, it is not part of the structural model and it comes after the pin joint in the load path (Fig. 6). Could you elaborate on how the fuselage backup structure should be considered in this exercise?
- My understanding is that in the option 1 the focus of UQ is on the numerator of the reserve factor, the load. I would like to know if my understanding is correct and thus we can use the strenght of the pin connection as given in the document "calculation_example_simple_method" (without uncertainties).
Thank you and kind regards,
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Arianna Bosco
Dr
Siemens Industry Software
Munich
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Original Message:
Sent: 12 Mar, 2026 17:58
From: John Schaefer
Subject: Questions for March 19 Meeting on Structures
Hello Everyone,
You are hopefully aware by now that our next full community meeting is scheduled for Thursday, March 19 at 11:00 am US Eastern Time. The organizing team is aware that depending on your geographic location or conflicting commitments, not all of you will be able to attend live. To this end, we are planning to record the meeting.
The subject of the meeting will be on the structures aspect of the Challenge Problem. If you have a question that you would like to ask, but you will be unable to attend the meeting live, please post your question to this thread. Time permitting, we will attempt to address these questions during the meeting so that you will be able to hear the answers when watching the recording later.
Thanks!
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John Schaefer
Associate Technical Fellow, Aerodynamics Engineer
The Boeing Company
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