Back to results

University of Illinois at Urbana-Champaign

High-fidelity aero-structural optimization framework for transonic aircraft design

dc:creator Ranjan, Prateek

thesis:degree_name Ph.D.

dc:date2022

Abstract

dc:description

Submission original under an indefinite embargo labeled 'Open Access'. The submission was exported from vireo on 2023-04-12 without embargo terms

Degree

thesis:*

Name thesis:degree_name: Ph.D.
Level thesis:degree_level: Dissertation
Discipline thesis:degree_discipline: Aerospace Engineering
Grantor: University of Illinois at Urbana-Champaign
Year dc:date: 2022

Author and committee

dc:creator, dc:contributor.*

Author dc:creator: Ranjan, Prateek
Contributors dc:contributor: Ansell, Phillip J
James, Kai A
Geubelle, Philippe H
Panesi, Marco
Magalhaes, Jose

Subjects

dc:subject × 4

Rights

dc:rights

Statement dc:rights: Copyright 2022 Prateek Ranjan
Language dc:language: en, eng

Identifiers

dc:identifier.*

Handle dc:identifier: https://hdl.handle.net/2142/117728
OAI identifier oai:identifier: oai:www.ideals.illinois.edu:2142/117728

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

related terms

citation

Ranjan, Prateek. High-fidelity aero-structural optimization framework for transonic aircraft design. Dissertation thesis, University of Illinois at Urbana-Champaign, 2022. https://hdl.handle.net/2142/117728

More from University of Illinois - Urbana-Champaign