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34th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, and AIAA/ASME Adaptive Structures Forum, La Jolla, CA, Apr. 19-22, 1993, Technical Papers. Pts. 1-6Topics addressed include the prediction of helicopter component loads using neural networks, spacecraft on-orbit coupled loads analysis, hypersonic flutter of a curved shallow panel with aerodynamic heating, thermal-acoustic fatigue of ceramic matrix composite materials, transition elements based on transfinite interpolation, damage progression in stiffened composite panels, a direct treatment of min-max dynamic response optimization problems, and sources of helicopter rotor hub inplane shears. Also discussed are dynamics of a layered elastic system, confidence bounds on structural reliability, mixed triangular space-time finite elements, advanced transparency development for USAF aircraft, a low-velocity impact on a graphite/PEEK, an automated mode-tracking strategy, transonic flutter suppression by a passive flap, a nonlinear response of composite panels to random excitation, an optimal placement of elastic supports on a simply supported plate, a probabilistic assessment of composite structures, a model for mode I failure of laminated composites, a residual flexibility approach to multibody dynamics,and multilayer piezoelectric actuators.
Document ID
19930049879
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
American Institute of Aeronautics and Astronautics
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: 34th Structures, Structural Dynamics and Materials Conference
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/MSDM93
Subject Category
Structural Mechanics
Meeting Information
Meeting: AIAA/ASME Adaptive Structures Forum
Location: La Jolla, CA
Country: US
Start Date: April 19, 1993
End Date: April 22, 1993
Sponsors: American Society of Mechanical Engineers, American Institute of Aeronautics and Astronautics
Accession Number
93A33876
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.

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