Being Conservative with a Limited Number of Test Results

被引:7
作者
An, Jungeun [1 ]
Acar, Erdem [1 ]
Haftka, Raphael T. [1 ]
Kim, Nam H. [1 ]
Ifju, Peter G. [1 ]
Johnson, Theodore F. [2 ]
机构
[1] Univ Florida, Dept Mech & Aerosp Engn, Gainesville, FL 32611 USA
[2] NASA, Langley Res Ctr, Hampton, VA 23681 USA
来源
JOURNAL OF AIRCRAFT | 2008年 / 45卷 / 06期
关键词
D O I
10.2514/1.35551
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In aircraft structural design, failure stresses are obtained from coupon tests and then used to predict failure under combined loads in structural elements. Structural element tests are next used to update the failure envelope for combined loads. It is a common practice to repeat the element tests and then select the lowest test result as a conservative estimate of the mean failure stress. This practice is equivalent to reducing the average test failure stress by a knockdown factor (one that is quite variable). Instead, we propose using the average test result with an explicit knockdown factor obtained from statistical distribution of the test data. We show reductions in the variability of the estimated mean failure stress as well as the likelihood of unconservative estimate. In addition, when the initial distribution or confidence interval of the mean failure stresses is available, we can further decrease the chance of unconservative estimate using Bayesian updating. We demonstrate the gains associated with Bayesian updating when the upper and lower bounds of errors in the analytical predictions are available. Examples with uniform and lognormal distributions of failure stresses compare the lowest-result approach with the two alternatives with the explicit knockdown factor. Both approaches significantly reduce the likelihood of unconservative estimates of the mean failure stress. The average approach reduced this likelihood by about a half and the Bayesian approach by up to an order of magnitude (from 12.5 to 1%). We also examine scenarios in which estimates of error and variability are substantially inaccurate. We show that, even then, the likelihood of unconservalive estimates reduces significantly. Remarkably, an underestimate of variability also results in about a 2% higher average of the estimated mean failure stress. Thus, we are able to simultaneously use higher average failure stress (leading to lower weight) and reduce the likelihood of unconservative estimates.
引用
收藏
页码:1969 / 1975
页数:7
相关论文
共 10 条
[1]   Comparing effectiveness of measures that improve aircraft structural safety [J].
Acar, E. ;
Kale, A. ;
Haftka, R. T. .
JOURNAL OF AEROSPACE ENGINEERING, 2007, 20 (03) :186-199
[2]   Structural safety measures for airplanes [J].
Acar, E ;
Kale, A ;
Haftka, RT ;
Stroud, WJ .
JOURNAL OF AIRCRAFT, 2006, 43 (01) :30-38
[3]  
AEAR E, 2007, 48 AIAA ASME ASCE AH
[4]  
[Anonymous], 1965, NASA
[5]   ESTIMATION OF THE GENERALIZED EXTREME-VALUE DISTRIBUTION BY THE METHOD OF PROBABILITY-WEIGHTED MOMENTS [J].
HOSKING, JRM ;
WALLIS, JR ;
WOOD, EF .
TECHNOMETRICS, 1985, 27 (03) :251-261
[6]  
LINCOLN JW, 1980, TR805035 AER SYST DI
[7]  
LONG MW, 1999, DODFAAAR992
[8]  
WIRSCHING PH, 1992, PROBABILISTIC STRUCT, V3
[9]   Evaluation of failure criteria for fiber composites using finite element micromechanics [J].
Zhu, H ;
Sankar, BV ;
Marrey, RV .
JOURNAL OF COMPOSITE MATERIALS, 1998, 32 (08) :766-782
[10]  
1997, AIR5080 SOC AUT ENG