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Heat transfer measurements for Stirling machine cylindersThe primary purpose of this study was to measure the effects of inflow-produced heat turbulence on heat transfer in Stirling machine cylinders. A secondary purpose was to provide new experimental information on heat transfer in gas springs without inflow. The apparatus for the experiment consisted of a varying-volume piston-cylinder space connected to a fixed volume space by an orifice. The orifice size could be varied to adjust the level of inflow-produced turbulence, or the orifice plate could be removed completely so as to merge the two spaces into a single gas spring space. Speed, cycle mean pressure, overall volume ratio, and varying volume space clearance ratio could also be adjusted. Volume, pressure in both spaces, and local heat flux at two locations were measured. The pressure and volume measurements were used to calculate area averaged heat flux, heat transfer hysteresis loss, and other heat transfer-related effects. Experiments in the one space arrangement extended the range of previous gas spring tests to lower volume ratio and higher nondimensional speed. The tests corroborated previous results and showed that analytic models for heat transfer and loss based on volume ratio approaching 1 were valid for volume ratios ranging from 1 to 2, a range covering most gas springs in Stirling machines. Data from experiments in the two space arrangement were first analyzed based on lumping the two spaces together and examining total loss and averaged heat transfer as a function of overall nondimensional parameter. Heat transfer and loss were found to be significantly increased by inflow-produced turbulence. These increases could be modeled by appropriate adjustment of empirical coefficients in an existing semi-analytic model. An attempt was made to use an inverse, parameter optimization procedure to find the heat transfer in each of the two spaces. This procedure was successful in retrieving this information from simulated pressure-volume data with artificially generated noise, but it failed with the actual experimental data. This is evidence that the models used in the parameter optimization procedure (and to generate the simulated data) were not correct. Data from the surface heat flux sensors indicated that the primary shortcoming of these models was that they assumed turbulence levels to be constant over the cycle. Sensor data in the varying volume space showed a large increase in heat flux, probably due to turbulence, during the expansion stroke.
Document ID
19950009548
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Kornhauser, Alan A.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Kafka, B. C.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Finkbeiner, D. L.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Cantelmi, F. C.
(Virginia Polytechnic Inst. and State Univ. Blacksburg, VA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1994
Subject Category
Energy Production And Conversion
Report/Patent Number
NAS 1.26: 197128
NASA-CR-197128
Accession Number
95N15963
Funding Number(s)
CONTRACT_GRANT: NAG3-1285
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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