CaltechAUTHORS
  A Caltech Library Service

Detonations in Hydrocarbon Fuel Blends

Austin, J. M. and Shepherd, J. E. (2000) Detonations in Hydrocarbon Fuel Blends. California Institute of Technology , Pasadena, CA. (Unpublished) http://resolver.caltech.edu/CaltechAUTHORS:20141111-151235060

[img]
Preview
PDF - Submitted Version
See Usage Policy.

370Kb

Use this Persistent URL to link to this item: http://resolver.caltech.edu/CaltechAUTHORS:20141111-151235060

Abstract

A study of detonations in high molecular weight hydrocarbon fuels was performed in two GALCIT facilities: the 280 mm gaseous detonation tube (GDT) and a 1180 liter vessel (HYJET) with jet initiation capability. In the GDT, detonation pressure, wave speed and cell width measurements were made in hexane-oxygen-nitrogen mixtures with and without the addition of lower molecular weight fuels. Stoichiometric mixtures of hexane-oxygen were studied with nitrogen dilution varying from fuel-oxygen to fuel-air. Hexane-air mixtures were investigated with varying fractions of lower molecular weight fuels (hydrogen, acetylene, ethylene, and carbon monoxide). The measured cell width decreased indicating increased sensitivity to detonation with increasing fraction of hydrogen, acetylene, and ethylene, in order of effectiveness. The addition of a small fraction of carbon monoxide produced a small decrease in the cell width, but addition of more than about 75 % (by fuel mass) carbon monoxide resulted in a rapid increase in cell width. As the oxidation of carbon monoxide is extremely sensitive to the presence of hydrogenous species, cell width measurements were made in carbon monoxide-air mixtures with the addition of hydrogen or hydrocarbons of various H-atom content and structure (acetylene, ethylene, and hexane). A detonation could be initiated in mixtures with very small fraction of hexane (0.07% of the mixture volume). Cell width measurements were compared to calculated ZND reaction zone parameters, including temperature and radical species concentrations. It was determined that for addition of hydrogen, ethylene or hexane, the cell width can be correlated with the product of the peak OH and CO concentrations in the reaction zone. Mixtures containing acetylene also showed the same linear dependance on this parameter, but, for the same peak OH and CO concentration, the cell widths were a factor of two smaller than those of the other mixtures. A fuel blend representative of thermally decomposed JP-10 was studied at 295 K. This blend consisted of hydrogen, carbon monoxide, methane, acetylene, ethylene, and hexane with varying fractions of oxygen and nitrogen. The cell width for stoichiometric fuel blend-oxygen was found to be an order of magnitude smaller than that for fuel blend-air. The cell width for the fuel blend-air mixture was about half that of hexane-air. Further experiments were carried out in the HYJET facility. A hydrogen-oxygen-nitrogen jet was used to initiate detonations in vapor phase mixtures of hexane (at 295 K) and of dodecane (at 380 K) with stoichiometric oxygen. Pressure and wave speed measurements were made. A critical nitrogen dilution limit was determined for each fuel. The critical limit was found to be 2.5 ≤ β ≤ 3.0 for hexane, where β is the ratio of nitrogen to oxygen concentration. This corresponds to a D/λ (nozzle diameter/cell width) ratio of 4, which compares well with the value 4.3 previously determined for this driver. The critical nitrogen dilution limit for dodecane was also found to be 2.5 ≤ β ≤ 3.0. No cell width measurements are currently available for dodecane. An attempt was made to initiate detonation in a dodecane spray. Pressure and velocity measurements were made and clearly show that no detonation could be directly initiated. Different fuel injection systems were tried and the initial temperature of the mixture was varied.


Item Type:Report or Paper (Technical Report)
ORCID:
AuthorORCID
Shepherd, J. E.0000-0003-3181-9310
Additional Information:© 2000 California Institute of Technology. Explosion Dynamics Laboratory Report FM99-6. Prepared for the Air Force and Advanced Projects Research Inc., under contract F04611-98-C-0046.
Group:Graduate Aeronautical Laboratories (Fluid Mechanics), GALCIT
Funders:
Funding AgencyGrant Number
Air Force Office of Scientific Research (AFOSR)F04611-98-C-0046
Other Numbering System:
Other Numbering System NameOther Numbering System ID
GALCITFM99-6
Record Number:CaltechAUTHORS:20141111-151235060
Persistent URL:http://resolver.caltech.edu/CaltechAUTHORS:20141111-151235060
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:51605
Collection:CaltechGALCITFM
Deposited By: Kristin Buxton
Deposited On:11 Nov 2014 23:20
Last Modified:22 Sep 2016 22:37

Repository Staff Only: item control page