Show simple item record

dc.contributor.advisor Dowell, Earl H en_US
dc.contributor.author Bloomhardt, EM
dc.contributor.author Dowell, EH
dc.date.accessioned 2012-05-29T16:36:36Z
dc.date.issued 2011
dc.identifier.citation Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2011
dc.identifier.issn 0273-4508
dc.identifier.uri http://hdl.handle.net/10161/5615
dc.description Thesis en_US
dc.description.abstract In support of the noise reduction targets for future generations of transport aircraft, as set forth by NASA, the fundamental aeroelastic behavior of trailing edge flap technology was explored. Using a plate structural model to approximate the structural configuration and linear potential flow theory to represent the aerodynamics, aeroelastic behavior was characterized for two structural configurations: all edges simply supported and leading and side edges simply supported trailing edge free. Results are compared to calculations presented in the literature for all edges simply supported configurations. Copyright © 2011 by the American Institute of Aeronautics and Astronautics, Inc.
dc.language eng
dc.relation.ispartof Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
dc.relation.isversionof 10.2514/6.2011-1995
dc.title A study of the aeroelastic behavior of flat plates and membranes with mixed boundary conditions in axial subsonic flow
dc.type Journal Article
dc.department Mechanical Engineering and Materials Science en_US
pubs.organisational-group /Duke
pubs.organisational-group /Duke/Pratt School of Engineering
pubs.organisational-group /Duke/Pratt School of Engineering/Mechanical Engineering and Materials Science

Files in this item

This item appears in the following Collection(s)

Show simple item record