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contributor authorF. Sisto
contributor authorA. Chang
contributor authorM. Sutcu
date accessioned2017-05-08T23:15:34Z
date available2017-05-08T23:15:34Z
date copyrightApril, 1983
date issued1983
identifier issn1528-8919
identifier otherJETPEZ-26781#342_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/97105
description abstractTurbomachine blades on spinning and precessing rotors experience gyroscopically induced instabilities and forcing. With vehicle-mounted turbomachines, either constant or harmonic precession occurs, depending on vehicle or mount motion. Responses of uniform cantilever beams at arbitrary stagger, subjected to the noted rotor motion, are predicted in both self-excited and forced-excitation modes taking into account Coriolis acceleration.
publisherThe American Society of Mechanical Engineers (ASME)
titleThe Influence of Coriolis Forces on Gyroscopic Motion of Spinning Blades
typeJournal Paper
journal volume105
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3227421
journal fristpage342
journal lastpage347
identifier eissn0742-4795
keywordsMotion
keywordsCoriolis force
keywordsSpin (Aerodynamics)
keywordsBlades
keywordsTurbomachinery
keywordsRotors
keywordsVehicles AND Cantilever beams
treeJournal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 002
contenttypeFulltext


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