AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 33rd, Dallas, TX, Apr. 13-15, 1992, Technical Papers. Pt. 4 - Structural dynamics II
The present conference discusses composites damage tolerance, shell and cylinder buckling, computational structural mechanics, adaptive structures, structural risk and reliability, the analysis of composite structures, the thermal analysis of structures, the finite-element analysis of rotorcraft vibration, spacecraft dynamics, and rotor aeroelasticity. Also discussed are rotorcraft dynamics, structural damping, control analyses and control experiments, dynamic methods, experimental dynamics and testing, composite structural dynamics and damage, aeroelasticity, future directions in flight mechanics and structures, rotorcraft aeroelasticity, dynamics applications, unsteady aerodynamics, eigensolution methods, nonlinear dynamics, sensitivity analysis and topology optimization, shape optimization, modeling of material behavior, and ceramic-matrix composites.
- OSTI ID:
- 7281301
- Report Number(s):
- CONF-920499--
- Country of Publication:
- United States
- Language:
- English
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AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 33rd, Dallas, TX, Apr. 13-15, 1992, Technical Papers. Pt. 5 - Design engineering/design optimization, materials, work-in-progress
AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 33rd, Dallas, TX, Apr. 13-15, 1992, Technical Papers. Pt. 3 - Structural dynamics I
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ABSTRACTS
AEROSPACE INDUSTRY
AIRCRAFT
CERAMICS
COMPOSITE MATERIALS
COMPUTERS
CONTROL SYSTEMS
DIGITAL COMPUTERS
DOCUMENT TYPES
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RELIABILITY
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