Research projects involving oscillatory combustion and fuel vaporization are reported. Comparisons of experimental and theoretical droplet vaporization histories under ambient conditions such that the droplet may approach its thermodynamic critical point are presented. Experimental data on instantaneous heat transfer from a gas to a solid surface under conditions of oscillatory pressure with comparisons to an unsteady one-dimensional model are analyzed. Droplet size and velocity distribution in a spray as obtained by use of a double flash fluorescent method were investigated
The goal of this research was to experimentally characterize the behavior of droplets in vaporizing ...
Measurements were made on the burning of liquid hydrazine, MMH, and UDMH in a combustion gas environ...
A project on droplet combustion, pursued jointly with F. L. Dryer of Princeton University, has now b...
Droplet vaporization in region of critical point in flowing stream and stagnant gas at high pressure...
A theoretical investigation was conducted on the open-loop combustion response of monopropellant dro...
An earlier analysis for the combustion response of a liquid monopropellant strand (hydrazine) was ex...
Fuel droplets were simulated by porous spheres having diameters in the range 0.63 to 1.9 cm and comb...
Detailed measurements were made of the structures of turbulent fuel sprays vaporizing in heated airs...
The combustion and evaporation of liquid fuels at high pressures were investigated. Particular empha...
The steady combustion characteristics of droplets were considered in combustion chamber environments...
A project on droplet combustion, pursued jointly with F.L. Dryer of Princeton University, has now be...
The general problem of spray combustion was investigated. The combustion of bipropellent droplets; c...
Steady and unsteady combustion of liquid fuel droplets under rocket engine conditions was analyzed. ...
Depending on the surrounding flow and thermodynamic conditions, a single droplet may experience seve...
A numerical computing procedure was developed for calculating vaporization histories of evaporating ...
The goal of this research was to experimentally characterize the behavior of droplets in vaporizing ...
Measurements were made on the burning of liquid hydrazine, MMH, and UDMH in a combustion gas environ...
A project on droplet combustion, pursued jointly with F. L. Dryer of Princeton University, has now b...
Droplet vaporization in region of critical point in flowing stream and stagnant gas at high pressure...
A theoretical investigation was conducted on the open-loop combustion response of monopropellant dro...
An earlier analysis for the combustion response of a liquid monopropellant strand (hydrazine) was ex...
Fuel droplets were simulated by porous spheres having diameters in the range 0.63 to 1.9 cm and comb...
Detailed measurements were made of the structures of turbulent fuel sprays vaporizing in heated airs...
The combustion and evaporation of liquid fuels at high pressures were investigated. Particular empha...
The steady combustion characteristics of droplets were considered in combustion chamber environments...
A project on droplet combustion, pursued jointly with F.L. Dryer of Princeton University, has now be...
The general problem of spray combustion was investigated. The combustion of bipropellent droplets; c...
Steady and unsteady combustion of liquid fuel droplets under rocket engine conditions was analyzed. ...
Depending on the surrounding flow and thermodynamic conditions, a single droplet may experience seve...
A numerical computing procedure was developed for calculating vaporization histories of evaporating ...
The goal of this research was to experimentally characterize the behavior of droplets in vaporizing ...
Measurements were made on the burning of liquid hydrazine, MMH, and UDMH in a combustion gas environ...
A project on droplet combustion, pursued jointly with F. L. Dryer of Princeton University, has now b...