Repository logo
Log in(current)
Repository logoMIT Open ScholarshipDSpace@MIT
  1. Home
  2. MIT Open Access Articles
  3. MIT Open Access Articles
  4. Variance-Based Sensitivity Analysis to Support Simulation-Based Design Under Uncertainty

Variance-Based Sensitivity Analysis to Support Simulation-Based Design Under Uncertainty

Thumbnail Image
Download
Name

Variance-based.pdf

Size

1.05 MB

Format

Adobe PDF

Checksum (MD5)

d05b052c4f41bb9d2c229088ee2a8653

Author(s)
Allaire, Douglas L.
•
Opgenoord, Max Maria Jacques
•
Willcox, Karen E
Date Issued
September 2016
Journal
Journal of Mechanical Design
Publisher
ASME International
Citation
Opgenoord, Max M. J., Douglas L. Allaire, and Karen E. Willcox. “Variance-Based Sensitivity Analysis to Support Simulation-Based Design Under Uncertainty.” Journal of Mechanical Design 138.11 (2016): 111410. © 2016 by ASME
Version
Final published version
Abstract
Sensitivity analysis plays a critical role in quantifying uncertainty in the design of engineering systems. A variance-based global sensitivity analysis is often used to rank the importance of input factors, based on their contribution to the variance of the output quantity of interest. However, this analysis assumes that all input variability can be reduced to zero, which is typically not the case in a design setting. Distributional sensitivity analysis (DSA) instead treats the uncertainty reduction in the inputs as a random variable, and defines a variance-based sensitivity index function that characterizes the relative contribution to the output variance as a function of the amount of uncertainty reduction. This paper develops a computationally efficient implementation for the DSA formulation and extends it to include distributions commonly used in engineering design under uncertainty. Application of the DSA method to the conceptual design of a commercial jetliner demonstrates how the sensitivity analysis provides valuable information to designers and decision-makers on where and how to target uncertainty reduction efforts.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
Article is made available in accordance with the publisher's policy and may be subject to US copyright law. Please refer to the publisher's site for terms of use.
Persistent DSpace Link
http://hdl.handle.net/1721.1/106283
DOI of Published Version
https://doi.org/10.1115/1.4034224
Repository logo
PrivacyPermissionsAccessibilityContact us
Repository logo
Notify us about copyright concerns.