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Statistical Evaluation and Improvement of Methods for Combining Random and Harmonic LoadsStructures in many environments experience both random and harmonic excitation. A variety of closed-form techniques has been used in the aerospace industry to combine the loads resulting from the two sources. The resulting combined loads are then used to design for both yield/ultimate strength and high- cycle fatigue capability. This Technical Publication examines the cumulative distribution percentiles obtained using each method by integrating the joint probability density function of the sine and random components. A new Microsoft Excel spreadsheet macro that links with the software program Mathematica to calculate the combined value corresponding to any desired percentile is then presented along with a curve tit to this value. Another Excel macro that calculates the combination using Monte Carlo simulation is shown. Unlike the traditional techniques. these methods quantify the calculated load value with a consistent percentile. Using either of the presented methods can be extremely valuable in probabilistic design, which requires a statistical characterization of the loading. Additionally, since the CDF at high probability levels is very flat, the design value is extremely sensitive to the predetermined percentile; therefore, applying the new techniques can substantially lower the design loading without losing any of the identified structural reliability.
Document ID
20030017832
Acquisition Source
Marshall Space Flight Center
Document Type
Technical Publication (TP)
Authors
Brown, A. M.
(NASA Marshall Space Flight Center Huntsville, AL United States)
McGhee, D. S.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Date Acquired
September 7, 2013
Publication Date
February 1, 2003
Subject Category
Engineering (General)
Report/Patent Number
M-1062
NASA/TP-2003-212257
NAS 1.60:212257
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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