A study of the aeroelastic behavior of flat plates and membranes with mixed boundary conditions in axial subsonic flow
Dowell, Earl H
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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.
Published Version (Please cite this version)10.2514/6.2011-1995
Publication InfoBloomhardt, EM; & Dowell, EH (2011). A study of the aeroelastic behavior of flat plates and membranes with mixed boundary conditions in axial subsonic flow. Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. 10.2514/6.2011-1995. Retrieved from https://hdl.handle.net/10161/5615.
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Rights for Collection: Masters Theses