TY - GEN
T1 - Enhanced deterministic performance of panels using stochastic variations of geometric and material parameters
AU - van den Broek, Sander
AU - Minera, Sergio
AU - Pirrera, Alberto
AU - Weaver, Paul M.
AU - Jansen, Eelco
AU - Rolfes, Raimund
N1 - Publisher Copyright:
© 2019 by German Aerospace Center (DLR). Published by the American Institute of Aeronautics and Astronautics, Inc.
PY - 2019
Y1 - 2019
N2 - The effect on structural performance of stochastic variation in material and geometric properties is important for robust design. Knowledge of such effects can be acquired by applying variation patterns to a structure using stochastic fields through a Monte Carlo analysis. The output is post-processed to show the correlation field between the stochastic variation of a structural property and a chosen mechanical response measure. The resulting patterns are used to identify areas most susceptible to variations, as well as areas which have the most potential to increase structural performance by varying the material parameter or geometry. This method is demonstrated on a flat plate and curved panel, by either varying the Young’s modulus, or thickness of the structure to increase the linear buckling load. In both of these variations the average property is set to remain the same as the original structure. Applying the redistribution increased the linear buckling load by 9-42%.
AB - The effect on structural performance of stochastic variation in material and geometric properties is important for robust design. Knowledge of such effects can be acquired by applying variation patterns to a structure using stochastic fields through a Monte Carlo analysis. The output is post-processed to show the correlation field between the stochastic variation of a structural property and a chosen mechanical response measure. The resulting patterns are used to identify areas most susceptible to variations, as well as areas which have the most potential to increase structural performance by varying the material parameter or geometry. This method is demonstrated on a flat plate and curved panel, by either varying the Young’s modulus, or thickness of the structure to increase the linear buckling load. In both of these variations the average property is set to remain the same as the original structure. Applying the redistribution increased the linear buckling load by 9-42%.
UR - http://www.scopus.com/inward/record.url?scp=85083942541&partnerID=8YFLogxK
U2 - 10.2514/6.2019-0511
DO - 10.2514/6.2019-0511
M3 - Conference contribution
AN - SCOPUS:85083942541
SN - 9781624105784
T3 - AIAA Scitech 2019 Forum
BT - AIAA Scitech 2019 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Scitech Forum, 2019
Y2 - 7 January 2019 through 11 January 2019
ER -