Show simple item record

contributor authorY. B. Kim
contributor authorS. T. Noah
date accessioned2017-05-08T23:35:25Z
date available2017-05-08T23:35:25Z
date copyrightOctober, 1991
date issued1991
identifier issn1528-8919
identifier otherJETPEZ-26691#550_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/108491
description abstractThe periodic steady-state response of a high-pressure oxygen turbopump (HPOTP) of a space shuttle main engine (SSME), involving a clearance between the bearing and housing carrier, is sought. A harmonic balance method utilizing Fast Fourier Transform (FFT) algorithm is developed for the analysis. An impedance method is used to reduce the number of degrees of freedom to the displacements at the bearing clearance. Harmonic and subharmonic responses to imbalance for various system parameters are studied. The results show that the computational technique developed in this study is an effective and flexible method for determining the stable and unstable periodic response of complex rotor-housing systems with clearance-type nonlinearity.
publisherThe American Society of Mechanical Engineers (ASME)
titleSteady-State Analysis of a Nonlinear Rotor-Housing System
typeJournal Paper
journal volume113
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2906276
journal fristpage550
journal lastpage556
identifier eissn0742-4795
keywordsRotors
keywordsSteady state
keywordsClearances (Engineering)
keywordsBearings
keywordsFast Fourier transforms
keywordsOxygen
keywordsDegrees of freedom
keywordsAlgorithms
keywordsEngines
keywordsImpedance (Electricity) AND High pressure (Physics)
treeJournal of Engineering for Gas Turbines and Power:;1991:;volume( 113 ):;issue: 004
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record