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University of Illinois at Urbana-Champaign

Component-based design optimization of multirotor aircraft

Abstract

dc:description

Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2022-11-15 without embargo terms

Degree

thesis:*
Name thesis:degree_name
M.S.
Level thesis:degree_level
Thesis
Discipline thesis:degree_discipline
Mechanical Engineering
Grantor
University of Illinois at Urbana-Champaign
Year dc:date
2022

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Renkert, Philip
Contributors dc:contributor
  • Alleyne, Andrew

Subjects

dc:subject × 4

Rights

dc:rights
Statement dc:rights
  • Copyright 2022 Philip Renkert
Language dc:language
en, eng

Identifiers

dc:identifier.*
Handle dc:identifier
https://hdl.handle.net/2142/116249
OAI identifier oai:identifier
oai:www.ideals.illinois.edu:2142/116249

Chain of custody

source
Harvested from
University of Illinois - Urbana-Champaign
Base URL
www.ideals.illinois.edu/oai-pmh
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Renkert, Philip. Component-based design optimization of multirotor aircraft. Thesis thesis, University of Illinois at Urbana-Champaign, 2022. https://hdl.handle.net/2142/116249