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

Conference · Wed Jan 01 00:00:00 EST 1992

OSTI ID:7281301

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-
• Resource Relation: Conference: 33. structural dynamics and materials conference, Dallas, TX (United States), 13-15 Apr 1992
• Country of Publication: United States
• Language: English

Related Subjects

42 ENGINEERING
36 MATERIALS SCIENCE
33 ADVANCED PROPULSION SYSTEMS
MATERIALS
MEETINGS
MECHANICAL STRUCTURES
AEROSPACE INDUSTRY
AIRCRAFT
CERAMICS
COMPOSITE MATERIALS
CONTROL SYSTEMS
ENGINEERING
FAULT TOLERANT COMPUTERS
FINITE ELEMENT METHOD
LEADING ABSTRACT
MECHANICAL VIBRATIONS
OSCILLATION MODES
RELIABILITY
ROTORS
ABSTRACTS
COMPUTERS
DIGITAL COMPUTERS
DOCUMENT TYPES
INDUSTRY
NUMERICAL SOLUTION
420200* - Engineering- Facilities
Equipment
& Techniques
360000 - Materials
330600 - Advanced Propulsion Systems- Vehicle Design Factors