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contributor authorFrank Ivancic
contributor authorAnthony Palazotto
date accessioned2017-05-08T21:16:12Z
date available2017-05-08T21:16:12Z
date copyrightJanuary 2005
date issued2005
identifier other%28asce%290893-1321%282005%2918%3A1%288%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/45022
description abstractThis paper attempts to characterize the various methods that may be used in defining the vibration features of a plate dimensionally proportioned to represent a turbine compressor blade. The comparison is specifically devoted towards certain damping properties of a titanium plate coated with magnesium aluminate spinel (mag spinel). Two different coating thicknesses were tested:
publisherAmerican Society of Civil Engineers
titleExperimental Considerations for Determining the Damping Coefficients of Hard Coatings
typeJournal Paper
journal volume18
journal issue1
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(2005)18:1(8)
treeJournal of Aerospace Engineering:;2005:;Volume ( 018 ):;issue: 001
contenttypeFulltext


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