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Please use this identifier to cite or link to this item: http://hdl.handle.net/11375/18359
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DC FieldValueLanguage
dc.contributor.advisorDokainish-
dc.contributor.authorJagannath, D.V.-
dc.date.accessioned2015-10-08T17:29:11Z-
dc.date.available2015-10-08T17:29:11Z-
dc.date.issued1969-03-
dc.identifier.urihttp://hdl.handle.net/11375/18359-
dc.description.abstract<p> The present investigation deals with Gas Turbine Blade Vibrations. Literature on the techniques employed for experimental investigation of gas turbine blade vibration characteristics has been summarised. Various steps have been explained by reviewing the different techniques. Several causes for possible excitation of blades as well as damping methods to suppress the resulting vibrations are also included. Attempts were made to determine experimentally the natural frequencies of cantilever plates of thin uniform rectangular cross section, with and without pretwist. First natural frequency_ -of the plate without twist was in good agreement with the one calculated from the plate formula. Free vibration analysis of cantilever plates of thin uniform rectangular cross section is made. Finite Element Technique is used to determine the elastic and inertial properties of a fully compatible triangular element. Computed values of natural freqencies and mode shapes are compared with other analytical results. </p>en_US
dc.language.isoenen_US
dc.subjectturbineen_US
dc.subjectblade vibrationen_US
dc.subjectmeasurementen_US
dc.subjectvibration analysisen_US
dc.subjectnatural frequenciesen_US
dc.subjectanalyticen_US
dc.titleBlade Vibration Measurement Techniques and Vibration Analysis of Platesen_US
dc.contributor.departmentMechanical Engineeringen_US
dc.description.degreetypeThesisen_US
dc.description.degreeMaster of Engineering (ME)en_US
Appears in Collections:Open Access Dissertations and Theses

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