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Virginia Tech

A theory and method of predicting the stability derivatives Clᵦ, Clᵣ, Cn𝗉, and CY𝗉 for wings of arbitrary planform in subsonic flow

Abstract

dc:description.abstract

A theory and method have been developed and design change drawn, for the estimation of certain stability derivatives for wings of arbitrary platform in subsonic flow.

Degree

thesis:*
Name thesis:degree_name
Ph. D.
Level thesis:degree_level
doctoral
Discipline thesis:degree_discipline
Engineering Mechanics
Department dc:contributor.department
Engineering Mechanics
Grantor dc:publisher
Virginia Tech
Year dc:date.issued
1963

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Queijo, M. J.
Committee members dc:contributor.committeemember
  • Fletcher, Herman S.
  • Brown, Clinton E.

Rights

dc:rights
Statement dc:rights
  • In Copyright
Language dc:language.iso
en

Identifiers

dc:identifier.*
Dc Identifier Other
etd-08012012-040657
OAI identifier oai:identifier
oai:vtechworks.lib.vt.edu:10919/39007

Chain of custody

source
Harvested from
Virginia Tech
Base URL
vtechworks.lib.vt.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
related terms
citation

Queijo, M. J.. A theory and method of predicting the stability derivatives Clᵦ, Clᵣ, Cn𝗉, and CY𝗉 for wings of arbitrary planform in subsonic flow. doctoral thesis, Virginia Tech, 1963. http://hdl.handle.net/10919/39007