SAE Technical Paper Series 2007
DOI: 10.4271/2007-24-0006
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Direct Heat Loss to Combustion Chamber Walls in a D.I. Diesel Engine-Development of Measurement Technique and Evaluation of Direct Heat Loss to Cylinder Liner Wall

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Cited by 6 publications
(10 citation statements)
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“…1 Although the combustion gases move close to the liner in the late expansion stroke, the gas temperature is much lower (see Figure 5(a)). Sugihara et al 48 found that the heat transfer losses from the cylinder liner are 3.6%-4.8%, which agrees well with the present results. Consistent findings have also been revealed by other related studies.…”
Section: Distributions Of Heat Transfer Losses In Different Componentssupporting
confidence: 92%
“…1 Although the combustion gases move close to the liner in the late expansion stroke, the gas temperature is much lower (see Figure 5(a)). Sugihara et al 48 found that the heat transfer losses from the cylinder liner are 3.6%-4.8%, which agrees well with the present results. Consistent findings have also been revealed by other related studies.…”
Section: Distributions Of Heat Transfer Losses In Different Componentssupporting
confidence: 92%
“…Looking at a g for measured points C1 and C2, it is seen that the values peaked right after TDC and then soon declined. Based on the previously obtained results for the cylinder liner of this experimental engine, 20 it is assumed that the increase in the apparent local heat transfer coefficient is attributed to a greater heat flux resulting from the temperature increase of the unburned gas in the piston top land crevice due to compression of the gas by the expansion of the already burned combustion gas. The next increase in the apparent local heat transfer coefficient is seen after a crank angle of approximately 27°ATDC, which is presumably attributed to increased heat flux when the combustion gas reached the cylinder liner wall surface accompanying the descent of the piston.…”
Section: Apparent Local Heat Transfer Coefficientmentioning
confidence: 99%
“…The temperature scales of the vertical axis differ for the piston, cylinder liner, cylinder head and the intake/exhaust valves because the temperature ranges of these combustion chamber wall surfaces are all different. [18][19][20][21] For the piston, high temperatures were measured at the points around the inner circumference of the top surface and the upper part of the cavity side wall. 18 This was as a result of the contact with the hot combustion flame.…”
Section: Tftsmentioning
confidence: 99%
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