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First Order Reliability Application and Verification Methods for Semistatic StructuresEscalating risks of aerostructures stimulated by increasing size, complexity, and cost should no longer be ignored by conventional deterministic safety design methods. The deterministic pass-fail concept is incompatible with probability and risk assessments, its stress audits are shown to be arbitrary and incomplete, and it compromises high strength materials performance. A reliability method is proposed which combines first order reliability principles with deterministic design variables and conventional test technique to surmount current deterministic stress design and audit deficiencies. Accumulative and propagation design uncertainty errors are defined and appropriately implemented into the classical safety index expression. The application is reduced to solving for a factor that satisfies the specified reliability and compensates for uncertainty errors, and then using this factor as, and instead of, the conventional safety factor in stress analyses. The resulting method is consistent with current analytical skills and verification practices, the culture of most designers, and with the pace of semistatic structural designs.
Document ID
19970016101
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Verderaime, Vincent
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
August 17, 2013
Publication Date
April 1, 1994
Publication Information
Publisher: American Inst. of Aeronautics and Astronautics
Subject Category
Quality Assurance And Reliability
Report/Patent Number
NAS 1.15:112713
NASA-TM-112713
Meeting Information
Meeting: Structures, Structural Materials Conference
Location: Hilton Head, SC
Country: United States
Start Date: April 1, 1994
Sponsors: American Inst. of Aeronautics and Astronautics
Accession Number
97N71467
Distribution Limits
Public
Copyright
Public Use Permitted.
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