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contributor authorMihai C. Duta
contributor authorLeigh B. Lapworth
contributor authorMichelle S. Campobasso
contributor authorMichael B. Giles
date accessioned2017-05-09T00:19:56Z
date available2017-05-09T00:19:56Z
date copyrightJanuary, 2006
date issued2006
identifier issn1528-8919
identifier otherJETPEZ-26894#183_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133734
description abstractThis paper presents an adjoint analysis for three-dimensional unsteady viscous flows aimed at the calculation of linear worksum sensitivities involved in turbomachinery forced response predictions. The worksum values are normally obtained from linear harmonic flow calculations but can also be computed using the solution to the adjoint of the linear harmonic flow equations. The adjoint method has a clear advantage over the linear approach if used within a rotor forced vibration minimization procedure which requires the structural response to a large number of different flow excitation sources characterized by a unique frequency and interblade phase angle. Whereas the linear approach requires a number of linear flow calculations at least equal to the number of excitation sources, the adjoint method reduces this cost to a single adjoint solution for each structural mode of rotor response. A practical example is given to illustrate the dramatic computational saving associated with the adjoint approach.
publisherThe American Society of Mechanical Engineers (ASME)
titleAdjoint Harmonic Sensitivities for Forced Response Minimization
typeJournal Paper
journal volume128
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2031227
journal fristpage183
journal lastpage189
identifier eissn0742-4795
keywordsRotors
keywordsVibration
keywordsFlow (Dynamics)
keywordsTurbomachinery
keywordsBlades
keywordsEquations
keywordsDamping AND Design
treeJournal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 001
contenttypeFulltext


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