An evaluation was made on the effects of using antimisting kerosene (AMK) on the performance of the components from the fuel system and the combustor of current in service JT8D aircraft engines. The objectives were to identify if there were any problems associated with using antimisting kerosene and to determine the extent of shearing or degradation required to allow the engine components to achieve satisfactory operation. The program consisted of a literature survey and a test program which evaluated the antimisting kerosene fuel in laboratory and bench component testing, and assessed the performance of the combustor in a high pressure facility and in an altitude relight/cold ignition facility
The fuel chemical property influence on a gas turbine combustor was studied using 25 test fuels. Fue...
The performance of a single-can JT8D combustor was evaluated with Jet A and a high-aromatic diesel f...
The ignition characteristics of sprays, created by wind shear action, of Jet-A fuel containing polyi...
The effects of antimisting kerosene on the performance of the components from the fuel system and th...
The problems associated with blending of the AMK additive with Jet A, and the base fuel effects on A...
The effect of antimisting kerosene (AMK) flow characteristics on fan jet engines and the impact of d...
The results of a NACA investigation conducted over a period of several years to evaluate the anti-kn...
An analytical study and laboratory tests were conducted to assist NASA in determining the safety and...
Various parameters found to affect the flammability of antimisting kerosene (Jet A + polymer additiv...
Technologies are reviewed for improving the thermal stability of jet fuels, with reference to the ov...
The general outlook for aviation turbine fuels, the effect that broadening permissible aviation turb...
As part of a study of the effects of fuel composition on the combustor performance of a turbojet eng...
In order to meet rapidly growing demand for fuel, as well as address environmental concerns, the avi...
The breakup behavior and flammability of antimisting turbine fuels subjected to aerodynamic shear ar...
The inline filtration characteristics of freshly blended and degraded antimisting fuels (AMK) at low...
The fuel chemical property influence on a gas turbine combustor was studied using 25 test fuels. Fue...
The performance of a single-can JT8D combustor was evaluated with Jet A and a high-aromatic diesel f...
The ignition characteristics of sprays, created by wind shear action, of Jet-A fuel containing polyi...
The effects of antimisting kerosene on the performance of the components from the fuel system and th...
The problems associated with blending of the AMK additive with Jet A, and the base fuel effects on A...
The effect of antimisting kerosene (AMK) flow characteristics on fan jet engines and the impact of d...
The results of a NACA investigation conducted over a period of several years to evaluate the anti-kn...
An analytical study and laboratory tests were conducted to assist NASA in determining the safety and...
Various parameters found to affect the flammability of antimisting kerosene (Jet A + polymer additiv...
Technologies are reviewed for improving the thermal stability of jet fuels, with reference to the ov...
The general outlook for aviation turbine fuels, the effect that broadening permissible aviation turb...
As part of a study of the effects of fuel composition on the combustor performance of a turbojet eng...
In order to meet rapidly growing demand for fuel, as well as address environmental concerns, the avi...
The breakup behavior and flammability of antimisting turbine fuels subjected to aerodynamic shear ar...
The inline filtration characteristics of freshly blended and degraded antimisting fuels (AMK) at low...
The fuel chemical property influence on a gas turbine combustor was studied using 25 test fuels. Fue...
The performance of a single-can JT8D combustor was evaluated with Jet A and a high-aromatic diesel f...
The ignition characteristics of sprays, created by wind shear action, of Jet-A fuel containing polyi...