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AIAA-2006-2059 Reliability Based Aircraft Structural Design Pays Even with Limited Statistical Data
Being Conservative with a Limited Number of Test Results
Comparing Effectiveness of Measures That Improve Aircraft Structural Safety
INTERDISCIPLINARY TOPICS - Increasing Allowable Flight Loads by Improved Structural Modeling
Options for Using Test Data to Update Failure Stress AIAA Paper 2007-1971 CD-ROM Number 8
Reliability-Based Aircraft Structural Design Pays, Even with Limited Statistical Data
Reliability-Based Design of Representative Wing and Tail System Together with Structural Tests
Reliability-Based Structural Design of Aircraft Together with Future Tests
RELIABILITY ESTIMATION THROUGH GUIDED TAIL MODELING USING SUPPORT VECTOR MACHINES
Robust Design of Energy Absorbing Components Considering The Manufacturing Effects
Simultaneous Design of a Stiffened Fuselage Panel and Number of Structural Tests