|Table of Contents|

New method of experimental study on supercritical characteristic of single droplet fuel(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2011年01期
Page:
7-16
Research Field:
研究与设计
Publishing date:

Info

Title:
New method of experimental study on supercritical characteristic of single droplet fuel
Author(s):
ZHANG Meng-zheng1 XU Sheng-li2
1. Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
Keywords:
-
PACS:
V439-34
DOI:
-
Abstract:
The supercritical fluid concept and progress of experimental study on evaporation and combustion of a fuel drop suspended in the supercritical environment are described in this paper. The piston driver which could compress gas to arrive a homogeneous high pressure and high temperature is introduced to study the fuel drop behavior in sub- and supercritical environment. The principle of the piston driver and final state estimation of the compressed gas are discussed. Cinematography, shadowgraph and planar laser induced fluorescence (PLIF) are briefly introduced for flow-field visualization and OH-PLIF imaging. Tunable diode laser absorption system (TDLAS) was utilized for temperature measurement. In contrast to drop imaging, the technologies of pressure and temperature measurements are adopted to identify the sub-, trans- and supercritical environment. The shortcomings of piston driver are also discussed.

References:

[1]Wikipedia. Supercritical_fluid [M/OL]. [2011-01-26]. http://en.wikipedia.org.
[2]BELLAN J. Supercritical (and subcritical) fluid behavior and modeling: drops, streams, shear and mixing layers, jets and sprays[J]. Progress in Energy and Combustion Science, 2004, 26:329-366.
[3]OSCHWALD M, SMITH J J, BRANAM R, et al. Injection of fluids into a supercritical environment[J]. Combustion Science and Technology, 2006, 178: 49-58.
[4]BRZUSTOWSKI T A, NATARAJAN R. Combustion of aniline droplets at high pressure [J]. Can. J. Chem. Engng., 1966, 44: 194-201.
[5]NATARAJAN R, BRZUSTOWSKI T A. Some new obser- vations on combustion of hydrocarbon droplets at elevated pressures[J]. Combustion Science and Technology, 1970, 2: 259-269.
[6]SAVERY C W. Experimental study of the vapouration of droplet in a heated air at high pressure, NASA CR7254 [R]. USA: NASA, 1969.
[7]MATLOSZ R L, LEIPZIGEN S, TORDA T P. Investigation of liquid drop evapouration in a high temperature and high pressure environment[J]. Int. heat Mass Transfer. 1972, 15: 831-852.
[8]SATO J. Studies on droplet evapouration and combustion in a high pressure, AIAA 93-0813[R]. USA: AIAA, 1993.
[9]HARSTAD K, BELLAN J. Isolated fluid oxygen drop behavior influid hydrogen at rocket chamber pressures [J]. Int. J. Heat Mass Transfer, 1998, 41: 3537-3550.
[10]MORIN C, CHESNAU X, GOKALP I. Studies on the influence of pressure and evapouration of n-heptane droplets, ILASS-Europe [R]. [S. l.]: [s. n.], 1999.
[11]CANADA G S, FAETH G M. Burning rates at fuel droplet in high pressure[C]// 14th international symposium on combustion. Canada: [s. n.], 1973, 1345-1354.
[12]KODATA T, HIROYASU H. Combustion of a fuel droplet in supercritical gaseous environments[J]. International Symposium On Combustion ,1981, 18: 275-282.
[13] CHAUVEAU C, CHESNAU X, GOKALP I. High pressure vaporization and burning of methanol droplets in reduced gravity, AIAA 94-0430 [R]. USA: AIAA, 1994.

Memo

Memo:
-
Last Update: 1900-01-01