Author: J. M. Kuchta
Publisher:
ISBN:
Category : Gas dynamics
Languages : en
Pages : 22
Book Description
Hot Gas Ignition Temperatures of Hydrocarbon Fuel Vapor-air Mixtures
Author: J. M. Kuchta
Publisher:
ISBN:
Category : Gas dynamics
Languages : en
Pages : 22
Book Description
Publisher:
ISBN:
Category : Gas dynamics
Languages : en
Pages : 22
Book Description
Hot gas ignition temperatures of hydrocarbon fuel vapor-air mixtures
Author: Joseph M. Kuchta
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
Book Description
Laminar hot air jets of 1/8- to 3/4-inch diameter were used to determine the hot gas ignition temperatures of various combustible vapor-air mixtures. The combustibles were n-hexane, n-octane, n-decane, a hydrocarbon jet fuel (JP-6), and an adipate ester aircraft engine oil (MIL-L-7808). Minimum ignition temperatures occurred at a fuel to air weight ratio of about 0.5 and were not greatly sensitive to variations of fuel concentration. Moderate variations of jet velocity also had little influence on these ignition temperatures. However, these temperatures decreased with increase in heat source dimensions (jet diameter). The hot gas ignition temperatures of the combustibles were not necessarily much greater than corresponding autoignition and wire ignition temperatures when the size of the heat source and the ignition criterion were the same. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
Book Description
Laminar hot air jets of 1/8- to 3/4-inch diameter were used to determine the hot gas ignition temperatures of various combustible vapor-air mixtures. The combustibles were n-hexane, n-octane, n-decane, a hydrocarbon jet fuel (JP-6), and an adipate ester aircraft engine oil (MIL-L-7808). Minimum ignition temperatures occurred at a fuel to air weight ratio of about 0.5 and were not greatly sensitive to variations of fuel concentration. Moderate variations of jet velocity also had little influence on these ignition temperatures. However, these temperatures decreased with increase in heat source dimensions (jet diameter). The hot gas ignition temperatures of the combustibles were not necessarily much greater than corresponding autoignition and wire ignition temperatures when the size of the heat source and the ignition criterion were the same. (Author).
HOT GAS IGNITION TEMPERATURES OF HYDROCARBON FUEL VAPOR-AIR MIXTURES.
Author: United States. Bureau of Mines
Publisher:
ISBN:
Category :
Languages : en
Pages : 39
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 39
Book Description
Ignition by Hot Gases
Author: Marcel Vanpée
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 20
Book Description
Ignition of Combustible Mixtures by Laminar Jets of Hot Gases
Author: Marcel Vanpée
Publisher:
ISBN:
Category : Aluminum oxide
Languages : en
Pages : 96
Book Description
Publisher:
ISBN:
Category : Aluminum oxide
Languages : en
Pages : 96
Book Description
Basic Considerations in the Combustion of Hydrocarbon Fuels with Air
Author: Lewis Flight Propulsion Laboratory. Propulsion Chemistry Division
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 288
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 288
Book Description
Ignition Characteristics of Fuels and Lubricants
Author: Joseph M. Kuchta
Publisher:
ISBN:
Category : Fire prevention
Languages : en
Pages : 57
Book Description
Hot surface ignition temperature data are presented for n-hexane, n-octane, n-decane, JP-6 jet fuel and aircraft engine oils MIL-L-7808 (0-60-18) and H-1026 in various oxygen-nitrogen atmospheres (2.5 to 100 volume percent oxygen) under stagnant or near-stagnant flow conditions. Minimum ignition temperatures were found to increase with decreasing oxygen concentration. In vessel ignitions, these temperatures increased with decrease in fuel contact time and with increase in surface area/volume ratio. In wire ignitions, the minimum ignition temperatures increased with decrease in wire diameter, length/diameter ratio, and initial mixture temperature. Expressions were developed to define the ignition temperatures as a function of the above pertinent variables. Hot gas ignition temperatures of the above combustibles were also found to vary with the heat source diameter, for 1/8, 3/8 and 1/2-inch diameter jets. In oxidation studies with n-octane vapor air-mixtures, rates of pressure rise were found to vary as the 0.38 power of the fuel concentration (5 to 30 volume percent) and as the 1.4 power of the initial total pressure (0.6 to 13 psia) at temperatures between 428 and 536F. (Author).
Publisher:
ISBN:
Category : Fire prevention
Languages : en
Pages : 57
Book Description
Hot surface ignition temperature data are presented for n-hexane, n-octane, n-decane, JP-6 jet fuel and aircraft engine oils MIL-L-7808 (0-60-18) and H-1026 in various oxygen-nitrogen atmospheres (2.5 to 100 volume percent oxygen) under stagnant or near-stagnant flow conditions. Minimum ignition temperatures were found to increase with decreasing oxygen concentration. In vessel ignitions, these temperatures increased with decrease in fuel contact time and with increase in surface area/volume ratio. In wire ignitions, the minimum ignition temperatures increased with decrease in wire diameter, length/diameter ratio, and initial mixture temperature. Expressions were developed to define the ignition temperatures as a function of the above pertinent variables. Hot gas ignition temperatures of the above combustibles were also found to vary with the heat source diameter, for 1/8, 3/8 and 1/2-inch diameter jets. In oxidation studies with n-octane vapor air-mixtures, rates of pressure rise were found to vary as the 0.38 power of the fuel concentration (5 to 30 volume percent) and as the 1.4 power of the initial total pressure (0.6 to 13 psia) at temperatures between 428 and 536F. (Author).
Calculation Procedure for the Thermodynamic, Transport, and Flow Properties of the Combustion Products of a Hydrocarbon Fuel Mixture Burned in Air with Results for Ethylene-air and Methane-air Mixtures
Author: E. W. Leyhe
Publisher:
ISBN:
Category : Chemistry, Physical and theoretical
Languages : en
Pages : 114
Book Description
Publisher:
ISBN:
Category : Chemistry, Physical and theoretical
Languages : en
Pages : 114
Book Description
Self-ignition Temperatures and Flash Points of Some High-energy Fuels
Author: Barbara Pusanski
Publisher:
ISBN:
Category : Boron as fuel
Languages : en
Pages : 22
Book Description
Publisher:
ISBN:
Category : Boron as fuel
Languages : en
Pages : 22
Book Description
List of Publications
Author: United States. Bureau of Mines
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 824
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 824
Book Description