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Probabilistic Multi-Factor Interaction Model for Complex Material BehaviorThe Multi-Factor Interaction Model (MFIM) is used to evaluate the divot weight (foam weight ejected) from the launch external tanks. The multi-factor has sufficient degrees of freedom to evaluate a large number of factors that may contribute to the divot ejection. It also accommodates all interactions by its product form. Each factor has an exponent that satisfies only two points the initial and final points. The exponent describes a monotonic path from the initial condition to the final. The exponent values are selected so that the described path makes sense in the absence of experimental data. In the present investigation, the data used was obtained by testing simulated specimens in launching conditions. Results show that the MFIM is an effective method of describing the divot weight ejected under the conditions investigated.
Document ID
20080043611
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Chamis, Christos C.
(NASA Glenn Research Center Cleveland, OH, United States)
Abumeri, Galib H.
(Alpha STAR Corp. Long Beach, CA, United States)
Date Acquired
August 24, 2013
Publication Date
September 1, 2008
Subject Category
Composite Materials
Report/Patent Number
E-16478-1
NASA/TM-2008-215244
AIAA Paper 2008-1987
Report Number: E-16478-1
Report Number: NASA/TM-2008-215244
Report Number: AIAA Paper 2008-1987
Meeting Information
Meeting: 10th Non-Deterministic Approaches (NDA) Conference
Location: Schaumburg, IL
Country: United States
Start Date: April 7, 2008
End Date: April 10, 2008
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 561581.02.10.03.023
Distribution Limits
Public
Copyright
Public Use Permitted.
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