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contributor authorJ. R. Cummins
date accessioned2017-05-09T01:38:06Z
date available2017-05-09T01:38:06Z
date copyrightJuly, 1974
date issued1974
identifier issn1528-8919
identifier otherJETPEZ-26711#181_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/164737
description abstractTo investigate the sources of acoustic radiation from a gas turbine exhaust, a one-seventh scale model has been constructed. The model geometrically scales the flow path downstream of the rotating parts including support struts and turning vanes. A discussion and comparison of different kinds of aerodynamic and acoustic scaling techniques are given. The effect of the temperature ratio between model and prototype is found to be an important parameter in comparing acoustical data.
publisherThe American Society of Mechanical Engineers (ASME)
titleAcoustic Characteristics of a Gas Turbine Exhaust Model
typeJournal Paper
journal volume96
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3445791
journal fristpage181
journal lastpage184
identifier eissn0742-4795
keywordsAcoustics
keywordsGas turbines
keywordsExhaust systems
keywordsTurning vanes
keywordsEngineering prototypes
keywordsFlow (Dynamics)
keywordsTemperature AND Radiation (Physics)
treeJournal of Engineering for Gas Turbines and Power:;1974:;volume( 096 ):;issue: 003
contenttypeFulltext


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