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contributor authorJ. M. Vance
contributor authorB. T. Murphy
contributor authorH. A. Tripp
date accessioned2017-05-08T23:26:15Z
date available2017-05-08T23:26:15Z
date copyrightJanuary, 1987
date issued1987
identifier issn1048-9002
identifier otherJVACEK-28972#1_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/103350
description abstractThis is the first part (Part I) of two papers describing results of a research program directed at verifying computer programs used to calculate critical speeds of turbomachinery. This research program was undertaken since questions existed about the accuracy of calculations for the second and higher critical speeds. Part I describes improvements in computer programs and data modeling that resulted from comparing measured and calculated “free-free” natural frequencies of several shafts and rotors. Program modifications to improve accuracy include consideration of the effect of disk/shaft attachment stiffness, revised treatment of the end masses, and an improved convergence. Modifications resulting from the study are applicable to many other damped and undamped critical speed computer programs.
publisherThe American Society of Mechanical Engineers (ASME)
titleCritical Speeds of Turbomachinery: Computer Predictions vs. Experimental Measurements—Part I: The Rotor Mass—Elastic Model
typeJournal Paper
journal volume109
journal issue1
journal titleJournal of Vibration and Acoustics
identifier doi10.1115/1.3269389
journal fristpage1
journal lastpage7
identifier eissn1528-8927
keywordsMeasurement
keywordsRotors
keywordsComputers
keywordsTurbomachinery
keywordsComputer software
keywordsFrequency
keywordsStiffness
keywordsDisks AND Modeling
treeJournal of Vibration and Acoustics:;1987:;volume( 109 ):;issue: 001
contenttypeFulltext


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