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An Experimental Determination of Losses in a 3-Port Wave RotorWave rotors, used in a gas turbine topping cycle, offer a potential route to higher specific power and lower specific fuel consumption. In order to exploit this potential properly, it is necessary to have some realistic means of calculating wave rotor performance, taking losses into account, so that wave rotors can be designed for good performance. This in turn requires a knowledge of the loss mechanisms. The experiment reported here was designed as a statistical experiment to identify the losses due to finite passage opening time, friction, and leakage. For simplicity, the experiment used a 3-port, flow divider, wave cycle, but the results should be applicable to other cycles. A 12 inch diameter rotor was used, with two different lengths, 9 inches and 18 inches, and two different passage widths, 0.25 inch and 0.54 inch, 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. The fit shows that there will be an optimum passage width for a given wave rotor, since, as the passage width increases, friction losses decrease, but opening-time losses increase, and vice-versa. Leakage losses can be made small at reasonable gap sizes.
Document ID
19960015938
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wilson, Jack
(NYMA, Inc. Brook Park, OH United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1996
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:198456
NASA-CR-198456
E-10079
Meeting Information
Meeting: Turbo Expo 1996
Location: Birmingham, England
Country: United States
Start Date: June 10, 1996
End Date: June 13, 1996
Accession Number
96N22129
Funding Number(s)
CONTRACT_GRANT: NAS3-27186
PROJECT: RTOP 505-62-75
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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