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Heat-flux measurements for the rotor of a full-stage turbine. II - Description of analysis technique and typical time-resolved measurementsAn analytical technique for obtaining the time-resolved heat flux of a turbine blade is applied to the case of a TFE 731-2 hp full-stage rotating turbine. In order to obtain the heat flux values from the thin film gage temperature histories, a finite difference procedure is used to solve the heat equation with variable thermal properties. After setting out the data acquisition and analysis procedures, their application is illustrated for three midspan locations on the blade and operation at the design flow function. Results demonstrate that the magnitude of the heat flux fluctuation due to vane-balde interaction is large by comparison to the time-averaged heat flux at all investigated locations; FFT of a portion of the heat flux record illustrates that the dominant frequencies occur at the wake-cutting frequency and its harmonics.
Document ID
19860063408
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dunn, M. G.
(Calspan Corp. Buffalo, NY, United States)
George, W. K.
(Calspan Corp. Buffalo, NY, United States)
Rae, W. J.
(Calspan Corp. Buffalo, NY, United States)
Woodward, S. H.
(Calspan Corp. Buffalo, NY, United States)
Moller, J. C.
(Calspan Research Center Buffalo, NY, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
ASME PAPER 86-GT-78
Accession Number
86A48146
Funding Number(s)
CONTRACT_GRANT: NAG3-469
CONTRACT_GRANT: NAG3-581
Distribution Limits
Public
Copyright
Other

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