Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 56
Book Description
Elastic Moduli and Damping of Vibrational Modes of Aluminum/Silicon Carbide Composite Beams
Elastic Moduli and Damping of Vibrational Modes of Aluminum/Silicon Carbide Composite Beams
Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781722370954
Category :
Languages : en
Pages : 56
Book Description
Elastic and shear moduli were determined for two aluminum matrix composites containing 20 and 40 volume percent discontinuous silicon carbide, respectively, using transverse, longitudinal, and torsional vibrational modes of specimens prepared as thin beams. These moduli are consistent with those determined from stress-strain measurements. The damping factors for these modes were also determined. Thermal properties are used to show that part of the damping of transverse modes is caused by the transverse thermal currents discussed by C. Zener (thermo-elastic damping); this damping is frequency-dependent with a maximum damping factor of approximately 0.002. The remaining damping is frequency-independent, and has roughly similar values in transverse, longitudinal, and torsional modes: approximately 0.0001. Leidecker, Henning Goddard Space Flight Center...
Engine Structures
Author: NASA Technical Memorandum
Author: Applied Mechanics Reviews
Author: Scientific and Technical Aerospace Reports
Author: The Shock and Vibration Digest
Author: Energy Research Abstracts
Author: Ceramic Abstracts
Author: American Ceramic SocietyPublisher:
ISBN:
Category : Ceramics
Languages : en
Pages : 1000
Book Description
Author: