SAE Technical Paper Series 2019
DOI: 10.4271/2019-01-2185
|View full text |Cite
|
Sign up to set email alerts
|

Comparison of heat losses at the impingement point and in between two impingement points in a diesel engine using phosphor thermometry

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1

Citation Types

0
3
0

Year Published

2021
2021
2021
2021

Publication Types

Select...
2

Relationship

0
2

Authors

Journals

citations
Cited by 2 publications
(3 citation statements)
references
References 20 publications
0
3
0
Order By: Relevance
“…For the full load case depicted in Figure 4, the CFD predicts that peak heat fluxes at certain locations can approach 40 MW/m 2 during peak combustion impingement on the piston. While these values do exceed the typical estimated range for a 1D correlation, such as Hohenberg [26] or Woschni [27], which are averaged over the entire combustion chamber surface area, experimental results by Binder et al [28] using phosphor thermometry…”
Section: Fea Temperature Field Solutionsmentioning
confidence: 75%
See 1 more Smart Citation
“…For the full load case depicted in Figure 4, the CFD predicts that peak heat fluxes at certain locations can approach 40 MW/m 2 during peak combustion impingement on the piston. While these values do exceed the typical estimated range for a 1D correlation, such as Hohenberg [26] or Woschni [27], which are averaged over the entire combustion chamber surface area, experimental results by Binder et al [28] using phosphor thermometry…”
Section: Fea Temperature Field Solutionsmentioning
confidence: 75%
“…For the full load case depicted in Figure 4, the CFD predicts that peak heat fluxes at certain locations can approach 40 MW/m 2 during peak combustion impingement on the piston. While these values do exceed the typical estimated range for a 1D correlation, such as Hohenberg [26] or Woschni [27], which are averaged over the entire combustion chamber surface area, experimental results by Binder et al [28] using phosphor thermometry demonstrated that the location under impinging burning jets can experience heat flux exceeding 60 MW/m 2 . The extreme magnitude of the local heat fluxes on the surface of the low-thermal conductivity, low-heat capacity coating led to instantaneous surface temperatures exceeding 1100 K. The amplitude of the intracycle temperature swing exceeded 600K.…”
Section: Fea Temperature Field Solutionsmentioning
confidence: 76%
“…Imaging techniques such as laser-induced phosphorescence [11][12][13] or infrared photography 14,15 have been applied to investigate engine heat transfer. These techniques can detect two-dimensional temperature distributions with good spatial resolution, so they are advantageous in understanding the overall heat transfer situation.…”
Section: Introductionmentioning
confidence: 99%