|
|
|
|
| LEADER |
00000nam a22000003u 4500 |
| 001 |
b5665013 |
| 003 |
CoU |
| 005 |
20100211000000.0 |
| 006 |
m o d f |
| 007 |
cr ||||||||||| |
| 008 |
130211e19951201dcu o| f1|||||eng|d |
| 035 |
|
|
|a (TOE)ost152669
|
| 035 |
|
|
|a (TOE)152669
|
| 040 |
|
|
|a TOE
|c TOE
|
| 049 |
|
|
|a GDWR
|
| 072 |
|
7 |
|a 33
|2 edbsc
|
| 086 |
0 |
|
|a E 1.99: conf-9510144--2
|
| 086 |
0 |
|
|a E 1.99:sand--95-8723c
|
| 086 |
0 |
|
|a E 1.99: conf-9510144--2
|
| 088 |
|
|
|a sand--95-8723c
|
| 088 |
|
|
|a conf-9510144--2
|
| 245 |
0 |
4 |
|a The effect of TDC temperature and density on the liquid-phase fuel penetration in a D.I. Diesel engine
|h [electronic resource]
|
| 260 |
|
|
|a Washington, D.C. :
|b United States. Dept. of Energy ;
|a Oak Ridge, Tenn. :
|b distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy,
|c 1995.
|
| 300 |
|
|
|a 17 p. :
|b digital, PDF file.
|
| 336 |
|
|
|a text
|b txt
|2 rdacontent.
|
| 337 |
|
|
|a computer
|b c
|2 rdamedia.
|
| 338 |
|
|
|a online resource
|b cr
|2 rdacarrier.
|
| 500 |
|
|
|a Published through the Information Bridge: DOE Scientific and Technical Information.
|
| 500 |
|
|
|a 12/01/1995.
|
| 500 |
|
|
|a "sand--95-8723c"
|
| 500 |
|
|
|a " conf-9510144--2"
|
| 500 |
|
|
|a "DE96002486"
|
| 500 |
|
|
|a International fuels and lubricants meeting and exposition, Toronto (Canada), 16-19 Oct 1995.
|
| 500 |
|
|
|a Dec, J.E.; Espey, C.
|
| 520 |
3 |
|
|a A parametric study of the liquid-phase fuel penetration of evaporating Diesel fuel jets has been conducted in a directinjection Diesel engine using laser elastic-scatter imaging. The experiments were conducted in an optically accessible Diesel engine of the ̀̀heavy-dutỳ̀ size class at a representative medium speed (1200 rpm) operating condition. The density and temperature at TDC were varied systematically by adjusting the intake temperature and pressure. At all operating conditions the measurements show that initially the liquid fuel penetrates almost linearly with increasing crank angle until reaching a maximum length. Then, the liquid-fuel penetration length remains fairly constant although fuel injection continues. At a TDC density of 16.6 kg/m³ and a temperature of about 1000 K the maximum penetration length is approximately 23 mm. However, it varies significantly as TDC conditions are changed, with the liquid-length being less at higher temperatures and at higher densities. The corresponding apparent heat release rate plots are presented and the results of the liquid-phase fuel penetration are discussed with respect to the ignition delay and premixed bum fraction.
|
| 536 |
|
|
|b AC04-94AL85000.
|
| 650 |
|
7 |
|a Diesel Fuels.
|2 local.
|
| 650 |
|
7 |
|a Diesel Engines.
|2 local.
|
| 650 |
|
7 |
|a Combustion Control.
|2 local.
|
| 650 |
|
7 |
|a Fuel-air Ratio.
|2 local.
|
| 650 |
|
7 |
|a Combustion Kinetics.
|2 local.
|
| 650 |
|
7 |
|a Jets.
|2 local.
|
| 650 |
|
7 |
|a Parametric Analysis.
|2 local.
|
| 650 |
|
7 |
|a Nozzles.
|2 local.
|
| 650 |
|
7 |
|a Advanced Propulsion Systems.
|2 edbsc.
|
| 710 |
2 |
|
|a Sandia National Laboratories.
|4 res.
|
| 710 |
1 |
|
|a United States.
|b Department of Energy.
|4 spn.
|
| 710 |
1 |
|
|a United States.
|b Department of Energy.
|b Office of Scientific and Technical Information.
|4 dst.
|
| 856 |
4 |
0 |
|u http://www.osti.gov/servlets/purl/152669-kcPrvV/webviewable/
|z Online Access
|
| 907 |
|
|
|a .b56650139
|b 03-06-23
|c 12-20-09
|
| 998 |
|
|
|a web
|b 12-20-09
|c f
|d m
|e p
|f eng
|g dcu
|h 4
|i 3
|
| 956 |
|
|
|a Information bridge
|
| 999 |
f |
f |
|i 704e13c0-8fba-55a7-9618-0889a82e517f
|s e2a203e3-05f9-5ae7-adb3-262038a3a164
|
| 952 |
f |
f |
|p Can circulate
|a University of Colorado Boulder
|b Online
|c Online
|d Online
|e E 1.99: conf-9510144--2
|h Superintendent of Documents classification
|i web
|n 1
|
