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dc.creatorRay, Sourav
dc.date.accessioned2012-06-07T22:38:08Z
dc.date.available2012-06-07T22:38:08Z
dc.date.created1994
dc.date.issued1994
dc.identifier.urihttps://hdl.handle.net/1969.1/ETD-TAMU-1994-THESIS-R264
dc.descriptionDue to the character of the original source materials and the nature of batch digitization, quality control issues may be present in this document. Please report any quality issues you encounter to digital@library.tamu.edu, referencing the URI of the item.en
dc.descriptionIncludes bibliographical references.en
dc.description.abstractThis thesis is concerned with the measurement of non-linear (i.e. strain amplitude dependent) intrinsic material damping in continuous fiber reinforced metalmatrix composites. The particular MMC studied is a 4-ply, [O︢]S, (O = 0, 15, 30, 45, 60, 75 degree), P55Gr/Al-6061 composite. A popular method for measuring damping is the free-decay of flexural vibrations of a cantilevered beam. The strain field in a cantilevered beam is inhomogeneous. For materials whose damping is non-linear, the measured damping is not equal to the intrinsic material damping. Using an elementary algorithm developed by Lazan, we extract non-linear intrinsic material damping from non-linear specimen damping. In general, damping is a function of temperature, strain amplitude and strain rate. For the measurements reported herein, the range of these parameters is: [ ] where T is the absolute temperature, Er is the root strain and f is the frequency in Hz.en
dc.format.mediumelectronicen
dc.format.mimetypeapplication/pdf
dc.language.isoen_US
dc.publisherTexas A&M University
dc.rightsThis thesis was part of a retrospective digitization project authorized by the Texas A&M University Libraries in 2008. Copyright remains vested with the author(s). It is the user's responsibility to secure permission from the copyright holder(s) for re-use of the work beyond the provision of Fair Use.en
dc.subjectaerospace engineering.en
dc.subjectMajor aerospace engineering.en
dc.titleThe measurement of non-linear damping in metal-matrix compositesen
dc.typeThesisen
thesis.degree.disciplineaerospace engineeringen
thesis.degree.nameM.S.en
thesis.degree.levelMastersen
dc.type.genrethesisen
dc.type.materialtexten
dc.format.digitalOriginreformatted digitalen


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