Proceedings of the ASME Aerospace Division: Structures and Materials for Aerospace Vehicles, Adaptive Structures and Material Systems, Micro-electro-mechanical Systems (MEMS) : Invited Papers
American Society of Mechanical Engineers, 1996 - Technology & Engineering - 816 pages
Contains papers from three symposia at the November 1996 congress. Sections on structures and materials for aerospace vehicles, adaptive structures and material systems, and micro-electro-mechanical systems include section introductions, and present the latest research.
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An Interaction Integral Formulation for Computing Stress Intensity Factors
Flutter Control of StraightSwept Aircraft Wings Using Combined Feedback
On the Instability of Ductile Crack Growth
23 other sections not shown
active actuator aging analysis angle applied approach ASME assumed beam behavior blade boundary changes compared components composite compression considered constant crack crack growth crack tip curve damage damping deformation determined developed devices direction displacement dynamic edge effect elastic electric element energy Engineering equations example experimental experiments failure fatigue fiber field Figure finite flow force fracture frequency function given increase initial integral Journal laminate layer length load mass material matrix measured mechanical method mode normal obtained optical parameters performance phase physical piezoceramic piezoelectric plane plastic plate prediction presented problem Proceedings properties ratio reaction region represents Research respectively response sensor shape shear shown shows solution specimen stiffness strain strength stress structure surface Table temperature theory thermal thickness values vibration voltage