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Effect of shrink fits on threshold speeds of rotordynamic instability
dc.creator | Mir, MD. Mofazzal Hossain | |
dc.date.accessioned | 2012-06-07T23:06:43Z | |
dc.date.available | 2012-06-07T23:06:43Z | |
dc.date.created | 2001 | |
dc.date.issued | 2001 | |
dc.identifier.uri | https://hdl.handle.net/1969.1/ETD-TAMU-2001-THESIS-M565 | |
dc.description | Due 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.description | Includes bibliographical references (leaves 61-62). | en |
dc.description | Issued also on microfiche from Lange Micrographics. | en |
dc.description.abstract | An investigation of the effect of shrink fits on threshold speeds of rotordynamic instability has been performed. It is known that running rotors at supercritical speed can result in some rotordynamic problems (asynchronous whirling). One such problem is the whirl instability caused by internal friction in a built-up rotor. Unlike passing through a resonance, where the amplitude of vibration increases and then decreases, the vibration of an unstable system continually grows exponentially; experimentally the vibration becomes very large but bounded. This can transfer large amounts of energy to the rotor system and can cause bearing damage or failure. Therefore, it is very important to understand the mechanism and the causes of violent rotor oscillation due to internal damping and to include it in rotordynamic models to assess the stability of the system. The free-free rap tests were conducted at different interference fits. The free vibration responses were analyzed, in order to identify the nature of the damping in the system and quantify it. Running tests were conducted to determine the onset speed of instability experimentally. Finally, the onset speed of instability was predicted analytically using the model presented by Gunter and the rotordynamic computer code (XLTRC) and compared with the experimental values. | en |
dc.format.medium | electronic | en |
dc.format.mimetype | application/pdf | |
dc.language.iso | en_US | |
dc.publisher | Texas A&M University | |
dc.rights | This 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.subject | mechanical engineering. | en |
dc.subject | Major mechanical engineering. | en |
dc.title | Effect of shrink fits on threshold speeds of rotordynamic instability | en |
dc.type | Thesis | en |
thesis.degree.discipline | mechanical engineering | en |
thesis.degree.name | M.S. | en |
thesis.degree.level | Masters | en |
dc.type.genre | thesis | en |
dc.type.material | text | en |
dc.format.digitalOrigin | reformatted digital | en |
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