Add to ORKGCombustion characteristics of liquid propellant droplets in air at near critical and super- critical pressure
Liquid fuel combustion provides a major portion of the world's energy supply. In most practical comb...
A major portion of the energy produced in the world today comes from the combustion or burning of li...
The combustion of pressure atomized fuel sprays in high pressure stagnant air was studied. Measureme...
Experimental and theoretical results of critical pressure burning of fuel droplet
The steady combustion characteristics of droplets were considered in combustion chamber environments...
The general problem of spray combustion was investigated. The combustion of bipropellent droplets; c...
Liquid rocket propellant droplet burning rate and lifetimes in combustion chambe
Fuel droplets were simulated by porous spheres having diameters in the range 0.63 to 1.9 cm and comb...
Steady and unsteady combustion of liquid fuel droplets under rocket engine conditions was analyzed. ...
Measurements were made on the burning of liquid hydrazine, MMH, and UDMH in a combustion gas environ...
Droplet vaporization in region of critical point in flowing stream and stagnant gas at high pressure...
The combustion and evaporation of liquid fuels at high pressures were investigated. Particular empha...
An earlier analysis for the combustion response of a liquid monopropellant strand (hydrazine) was ex...
Measurements were made of the burning rates and liquid surface temperatures for a number of alcohol ...
This is a joint research program, pursued by investigators at the University of Tokyo, UCSD, and NAS...
Liquid fuel combustion provides a major portion of the world's energy supply. In most practical comb...
A major portion of the energy produced in the world today comes from the combustion or burning of li...
The combustion of pressure atomized fuel sprays in high pressure stagnant air was studied. Measureme...
Experimental and theoretical results of critical pressure burning of fuel droplet
The steady combustion characteristics of droplets were considered in combustion chamber environments...
The general problem of spray combustion was investigated. The combustion of bipropellent droplets; c...
Liquid rocket propellant droplet burning rate and lifetimes in combustion chambe
Fuel droplets were simulated by porous spheres having diameters in the range 0.63 to 1.9 cm and comb...
Steady and unsteady combustion of liquid fuel droplets under rocket engine conditions was analyzed. ...
Measurements were made on the burning of liquid hydrazine, MMH, and UDMH in a combustion gas environ...
Droplet vaporization in region of critical point in flowing stream and stagnant gas at high pressure...
The combustion and evaporation of liquid fuels at high pressures were investigated. Particular empha...
An earlier analysis for the combustion response of a liquid monopropellant strand (hydrazine) was ex...
Measurements were made of the burning rates and liquid surface temperatures for a number of alcohol ...
This is a joint research program, pursued by investigators at the University of Tokyo, UCSD, and NAS...
Liquid fuel combustion provides a major portion of the world's energy supply. In most practical comb...
A major portion of the energy produced in the world today comes from the combustion or burning of li...
The combustion of pressure atomized fuel sprays in high pressure stagnant air was studied. Measureme...