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contributor authorA. G. Holms
contributor authorA. J. Repko
date accessioned2017-05-08T23:41:20Z
date available2017-05-08T23:41:20Z
date copyrightSeptember, 1960
date issued1960
identifier issn0098-2202
identifier otherJFEGA4-27224#695_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111945
description abstractExperimental justification is presented for extending an existing rotating disk deformation theory-finite difference plastic flow calculation method to predicting the deformation and fracture of welded composite aircraft gas turbine wheels. Calculated deformations generally equaled but sometimes exceeded measured deformations. Fractures could be predicted for wheels containing no significant defects. Defects observed in fracture surfaces were incomplete penetration, incomplete fusion, porosity, and coarse columnar structure. Of these, incomplete penetration was significantly associated with losses in strength.
publisherThe American Society of Mechanical Engineers (ASME)
titleBurst Strengths and Deformations of Welded Composite Turbine Wheels as Related to Weld Quality and Plasticity Calculations
typeJournal Paper
journal volume82
journal issue3
journal titleJournal of Fluids Engineering
identifier doi10.1115/1.3662708
journal fristpage695
journal lastpage708
identifier eissn1528-901X
keywordsPlasticity
keywordsDeformation
keywordsComposite materials
keywordsTurbines
keywordsWheels
keywordsFracture (Process)
keywordsProduct quality
keywordsAircraft
keywordsPorosity
keywordsRotating Disks AND Gas turbines
treeJournal of Fluids Engineering:;1960:;volume( 082 ):;issue: 003
contenttypeFulltext


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