Flutter of rectangular simply supported panels at high supersonic speeds

The panel flutter analysis presented herein has been restricted to the problem of an isolated simply supported plate of uniform thickness. The same type of analysis can be applied, however, to other panel configurations. Clamped panels, integrally stiffened panels, arrays of panels, end others should be amenable to treatment by the model approach based on the static aerodynamic approximation.

Name thesis:degree_name

Master of Science

Level thesis:degree_level

masters

Discipline thesis:degree_discipline

Applied Mechanics

Department dc:contributor.department

Applied Mechanics

Grantor dc:publisher

Virginia Tech

Year dc:date.issued

1957

Author dc:creator

• Hedgepeth, John Mills

Chair dc:contributor.committeechair

• Frederick, Daniel

Committee members dc:contributor.committeemember

• Pardue, Louis A.
• Pletta, Dan H.
• Whittemore, John A.

Statement dc:rights

• In Copyright

Licence dc:rights.uri

• http://rightsstatements.org/vocab/InC/1.0/

Language dc:language.iso

en

Dc Identifier Other

etd-11072012-040239

OAI identifier oai:identifier

oai:vtechworks.lib.vt.edu:10919/45527