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NASA-LLIS-1223

Lessons Learned – Limitations of extended use of simplified modeling

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1998

Abstract: Description of Driving Event:
The basis of the Z1 ITS modeling strategy in the preliminary and conceptual design phases was a simplified beam element representation of the primary structure bulkheads and panels. This facilitated rapid, automated beam based stress analysis of the primary structure and decreased the design cycle time as well as manpower loading. The same model was used for both (1) the design dynamic-coupled load analysis and (2) the pre-test model and static test prediction analyses.
The pretest model analysis model produced poor correlation with the model test data. The correlation was improved by remodeling critical bulkheads and panels in greater detail using shell elements for the basic web and shell/beam elements for the upstanding ribs & flanges. Solid elements were also used where "plate" proportions did not exist. The increased fidelity of the post-test model led to improved correlation with the static test as well. However, the changes made to the model have forced a re-evaluation of the internal stresses both because of the change in model response and/or load paths. This re-evaluation came long after the design of the hardware was finalized and manufacturing completed. Any adverse findings from this re-evaluation could lead to costly retrofits or undesired limitations on hardware use during operations.
URI: https://yse.yabesh.ir/std/handle/yse/111754
Subject: Computer-Aided Design/Manufacturing/Engineering
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    NASA-LLIS-1223

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:48:22Z
date available2017-09-04T16:48:22Z
date copyright36088
date issued1998
identifier otherWHVEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/111754
description abstractDescription of Driving Event:
The basis of the Z1 ITS modeling strategy in the preliminary and conceptual design phases was a simplified beam element representation of the primary structure bulkheads and panels. This facilitated rapid, automated beam based stress analysis of the primary structure and decreased the design cycle time as well as manpower loading. The same model was used for both (1) the design dynamic-coupled load analysis and (2) the pre-test model and static test prediction analyses.
The pretest model analysis model produced poor correlation with the model test data. The correlation was improved by remodeling critical bulkheads and panels in greater detail using shell elements for the basic web and shell/beam elements for the upstanding ribs & flanges. Solid elements were also used where "plate" proportions did not exist. The increased fidelity of the post-test model led to improved correlation with the static test as well. However, the changes made to the model have forced a re-evaluation of the internal stresses both because of the change in model response and/or load paths. This re-evaluation came long after the design of the hardware was finalized and manufacturing completed. Any adverse findings from this re-evaluation could lead to costly retrofits or undesired limitations on hardware use during operations.
languageEnglish
titleNASA-LLIS-1223num
titleLessons Learned – Limitations of extended use of simplified modelingen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1998
contenttypefulltext
subject keywordsComputer-Aided Design/Manufacturing/Engineering
subject keywordsFlight Equipment
subject keywordsGround Equipment
subject keywordsHardware
subject keywordsIndependent Verification and Validation
subject keywordsPolicy & Planning
subject keywordsRisk Management/Assessment
subject keywordsSafety & Mission Assurance
subject keywordsTest & Verification
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