An Approximate Numerical Method for the Optimization of Flap Design for Maximum Lift Coefficient

Edwards, Thomas Ewing

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University of Illinois at Urbana-Champaign

An Approximate Numerical Method for the Optimization of Flap Design for Maximum Lift Coefficient

dc:creator Edwards, Thomas Ewing

thesis:degree_name Ph.D.

dc:date2014

Abstract

dc:description

Made available in DSpace on 2014-12-14T04:42:00Z (GMT). No. of bitstreams: 1 7524297.pdf: 4657836 bytes, checksum: efb3249ae596e00155e4ccd68a6957ff (MD5) Previous issue date: 1975

Degree

thesis:*

Name thesis:degree_name: Ph.D.
Level thesis:degree_level: Dissertation
Discipline thesis:degree_discipline: Aeronautical and Astronautical Engineering
Grantor: University of Illinois at Urbana-Champaign
Year dc:date: 2014

Author and committee

dc:creator, dc:contributor.*

Author dc:creator: Edwards, Thomas Ewing

Subjects

dc:subject × 1

Engineering, Aerospace

Rights

Language dc:language: eng

Identifiers

dc:identifier.*

Identifier: (UMI)AAI7524297
OAI identifier oai:identifier: oai:www.ideals.illinois.edu:2142/67458

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

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citation

Edwards, Thomas Ewing. An Approximate Numerical Method for the Optimization of Flap Design for Maximum Lift Coefficient. Dissertation thesis, University of Illinois at Urbana-Champaign, 2014. http://hdl.handle.net/2142/67458

An Approximate Numerical Method for the Optimization of Flap Design for Maximum Lift Coefficient

Abstract

Degree

Author and committee

Subjects

Rights

Identifiers

Chain of custody

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