Add to ORKGA preliminary analytical evaluation of the air and fuel specific-impulse characteristics of hydrogen, a-methylnapthalene, and graphite carbon has been made. Adiabatic constant-pressure combustion flame temperatures for each fuel at several equivalence ratios were calculated for an initial air temperature of 560 degrees R and a pressure of 2 atmospheres
As part of a study of the effects of fuel composition on the combustor performance of a turbojet eng...
An analytical investigation was made of the performance of isolated ram-jet engines in the flight Ma...
Various aspects of specific thrust in ramjet propulsion have been considered. It is shownthat while ...
The results of an analytical investigation of the theoretical air specific impulse performance and a...
An analytical evaluation of the air and fuel specific-impulse characteristics of magnesium, magnesiu...
A preliminary analytical evaluation of the air and fuel specific-impulse characteristics of hydrogen...
Report presents the summation of results obtained in the testing of fuels of various compositions an...
Hydrogen is the fuel of choice for hypersonic vehicles. Its main disadvantage is its low liquid and ...
The fuel chemical property influence on a gas turbine combustor was studied using 25 test fuels. Fue...
The ideal temperature rise due to the constant-pressure combustion of a methylene (CH sub 2) fuel wa...
The starting characteristics and combustion performance of slurry type fuels, consisting of 50 perce...
An analytical evaluation of the air and fuel specific-impulse characteristics of magnesium, magnesiu...
A fuel performance database of liquid hydrocarbons and aluminum-hydrocarbon fuels was compiled using...
An analytical investigation of the effects of fuel density and heating value on the cruising range o...
Combustion efficiencies obtained with gaseous methane were compared with reported data obtained with...
As part of a study of the effects of fuel composition on the combustor performance of a turbojet eng...
An analytical investigation was made of the performance of isolated ram-jet engines in the flight Ma...
Various aspects of specific thrust in ramjet propulsion have been considered. It is shownthat while ...
The results of an analytical investigation of the theoretical air specific impulse performance and a...
An analytical evaluation of the air and fuel specific-impulse characteristics of magnesium, magnesiu...
A preliminary analytical evaluation of the air and fuel specific-impulse characteristics of hydrogen...
Report presents the summation of results obtained in the testing of fuels of various compositions an...
Hydrogen is the fuel of choice for hypersonic vehicles. Its main disadvantage is its low liquid and ...
The fuel chemical property influence on a gas turbine combustor was studied using 25 test fuels. Fue...
The ideal temperature rise due to the constant-pressure combustion of a methylene (CH sub 2) fuel wa...
The starting characteristics and combustion performance of slurry type fuels, consisting of 50 perce...
An analytical evaluation of the air and fuel specific-impulse characteristics of magnesium, magnesiu...
A fuel performance database of liquid hydrocarbons and aluminum-hydrocarbon fuels was compiled using...
An analytical investigation of the effects of fuel density and heating value on the cruising range o...
Combustion efficiencies obtained with gaseous methane were compared with reported data obtained with...
As part of a study of the effects of fuel composition on the combustor performance of a turbojet eng...
An analytical investigation was made of the performance of isolated ram-jet engines in the flight Ma...
Various aspects of specific thrust in ramjet propulsion have been considered. It is shownthat while ...