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contributor authorJ. Wilson
date accessioned2017-05-08T23:56:29Z
date available2017-05-08T23:56:29Z
date copyrightOctober, 1998
date issued1998
identifier issn1528-8919
identifier otherJETPEZ-26785#833_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/120377
description abstractWave rotors, used in a gas turbine topping cycle, offer a potential route to higher specific power and lower specific fuel consumption. In order to calculate this potential realistically, a knowledge of the loss mechanisms is required. The experiment reported here was designed as a statistical experiment to identify the losses due to finite passage opening time, friction, and leakage, using a three-port, flow divider, wave rotor cycle. Incidence loss was also found to be important. Rotors of 12 in. diameter were used, with two different lengths, 9 in. and 18 in., and two different passage widths, 0.25 in. and 0.54 in., in order to vary friction and opening time. To vary leakage, moveable end walls were provided so that the rotor to end wall gap could be adjusted. The experiment is described, and the results are presented, together with a parametric fit to the data.
publisherThe American Society of Mechanical Engineers (ASME)
titleAn Experimental Determination of Losses in a Three-Port Wave Rotor
typeJournal Paper
journal volume120
journal issue4
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2818476
journal fristpage833
journal lastpage842
identifier eissn0742-4795
keywordsWaves
keywordsRotors
keywordsCycles
keywordsLeakage
keywordsFriction
keywordsFlow (Dynamics)
keywordsGas turbines
keywordsFuel consumption AND Mechanisms
treeJournal of Engineering for Gas Turbines and Power:;1998:;volume( 120 ):;issue: 004
contenttypeFulltext


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