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Carleton University

High Fidelity and Efficient Computations of Dynamic Loads for Multidisciplinary Design Optimization of Flexible Transport Aircraft

Abstract

dc:description.abstract

The current state-of-the-art design optimization of airframes is tightly wounded to its loads analyses as the process is usually conducted employing a deterministic set of critical load cases. The sheer number of scenarios required to estimate the critical loading conditions prevent these two processes from integrating. In this thesis, we address the problem of an efficient estimation of critical dynamic aeroelastic loads. The method is based on the Kriging metamodeling technique and the Expected Improvement Function, known formally as the Efficient Global Optimization (EGO) algorithm. Furthermore, different inexpensive metrics, based on the concept of Modal Contribution Factors, are investigated as indicators to determine if a substantial change in the loads has occurred during the design optimization, triggering the re-exploration of the design space. A case study is presented to evaluate the performance of the proposed methodology, where a reduction of 84 percent in the total time of execution was achieved.

Degree

thesis:*
Name thesis:degree_name
Master of Applied Science (M.App.Sc.)
Level thesis:degree_level
Master's
Discipline thesis:degree_discipline
Engineering, Aerospace
Grantor dc:publisher
Carleton University
Year dc:date.issued
2018

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Guzman Nieto, Michelle

Rights

dc:rights
Statement dc:rights
  • Copyright © 2018 the author(s). Theses may be used for non-commercial research, educational, or related academic purposes only. Such uses include personal study, research, scholarship, and teaching. Theses may only be shared by linking to Carleton University Institutional Repository and no part may be used without proper attribution to the author. No part may be used for commercial purposes directly or indirectly via a for-profit platform; no adaptation or derivative works are permitted without consent from the copyright owner.
Language dc:language.iso
en

Identifiers

dc:identifier.*
OAI identifier oai:identifier
oai:carleton.scholaris.ca:20.500.14718/40516

Chain of custody

source
Harvested from
Carleton University
Base URL
carleton.scholaris.ca/server/oai/request
Last updated
2026-07-24
Source record
OAI-PMH GetRecord
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citation

Guzman Nieto, Michelle. High Fidelity and Efficient Computations of Dynamic Loads for Multidisciplinary Design Optimization of Flexible Transport Aircraft. Master's thesis, Carleton University, 2018. https://hdl.handle.net/20.500.14718/40516