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Methods for heat transfer and temperature field analysis of the insulated diesel, phase 3Work during Phase 3 of a program aimed at developing a comprehensive heat transfer and thermal analysis methodology for design analysis of insulated diesel engines is described. The overall program addresses all the key heat transfer issues: (1) spatially and time-resolved convective and radiative in-cylinder heat transfer, (2) steady-state conduction in the overall structure, and (3) cyclical and load/speed temperature transients in the engine structure. These are all accounted for in a coupled way together with cycle thermodynamics. This methodology was developed during Phases 1 and 2. During Phase 3, an experimental program was carried out to obtain data on heat transfer under cooled and insulated engine conditions and also to generate a database to validate the developed methodology. A single cylinder Cummins diesel engine was instrumented for instantaneous total heat flux and heat radiation measurements. Data were acquired over a wide range of operating conditions in two engine configurations. One was a cooled baseline. The other included ceramic coated components (0.050 inches plasma sprayed zirconia)-piston, head and valves. The experiments showed that the insulated engine has a smaller heat flux than the cooled one. The model predictions were found to be in very good agreement with the data.
Document ID
19890014011
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Morel, Thomas
(Ricardo-ITI Westmont, IL, United States)
Wahiduzzaman, Syed
(Ricardo-ITI Westmont, IL, United States)
Fort, Edward F.
(Ricardo-ITI Westmont, IL, United States)
Keribar, Rifat
(Ricardo-ITI Westmont, IL, United States)
Blumberg, Paul N.
(Ricardo-ITI Westmont, IL, United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1988
Subject Category
Urban Technology And Transportation
Report/Patent Number
NAS 1.26:182237
NASA-CR-182237
DOE/NASA/0342-3
Report Number: NAS 1.26:182237
Report Number: NASA-CR-182237
Report Number: DOE/NASA/0342-3
Accession Number
89N23382
Funding Number(s)
CONTRACT_GRANT: DE-AI01-86CE-50162
CONTRACT_GRANT: DEN3-342
PROJECT: RTOP 778-34-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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