Add to ORKGTheoretical studies of the turbojet and ramjet combustion process are summarized and the resulting equations are applied to experimental data obtained from various combustor tests. The theoretical treatment assumes that one step in the over-all chain of processes which constitute jet-engine combustion is sufficiently slow to be the rate-controlling step that determines combustion efficiency
Some of the systematic research conducted by the NACA on aircraft gas-turbine combustors is reviewed...
Research to develop high-speed airbreathing aerospace propulsion systems was underway in the late 19...
The results of an analytical investigation of the theoretical air specific impulse performance and a...
Theoretical studies of the turbojet and ramjet combustion process are summarized and the resulting e...
Combustion must be maintained in the turbojet-engine combustor over a wide range of operating condit...
The ram jet is basically one of the most dimple types of aircraft engine. It consists only of an inl...
An investigation was conducted t o determine the hrgortance of molecular-scale processes in the over...
Simplified chemical kinetic reaction mechanisms for the combustion of Jet A fuel was studied. Initia...
Based on the assumption that shock-free internal burning is possible in a supersonic airstream, calc...
Four different combustion efficiencies commonly used for assessing ramjet engines are compared. The ...
Results of a theoretical and experimental study of the total pressure losses and combustion efficien...
Successful modeling of combustion and emissions in gas turbine engine combustors requires an adequat...
Aerodynamic considerations in the design of high performance combustors for turbojet engines are dis...
As part of a general program to study combustion in the engine cylinder and to correlate the phenome...
Conducting full-scale experiments as part of the design process of jet engine combustors is a costly...
Some of the systematic research conducted by the NACA on aircraft gas-turbine combustors is reviewed...
Research to develop high-speed airbreathing aerospace propulsion systems was underway in the late 19...
The results of an analytical investigation of the theoretical air specific impulse performance and a...
Theoretical studies of the turbojet and ramjet combustion process are summarized and the resulting e...
Combustion must be maintained in the turbojet-engine combustor over a wide range of operating condit...
The ram jet is basically one of the most dimple types of aircraft engine. It consists only of an inl...
An investigation was conducted t o determine the hrgortance of molecular-scale processes in the over...
Simplified chemical kinetic reaction mechanisms for the combustion of Jet A fuel was studied. Initia...
Based on the assumption that shock-free internal burning is possible in a supersonic airstream, calc...
Four different combustion efficiencies commonly used for assessing ramjet engines are compared. The ...
Results of a theoretical and experimental study of the total pressure losses and combustion efficien...
Successful modeling of combustion and emissions in gas turbine engine combustors requires an adequat...
Aerodynamic considerations in the design of high performance combustors for turbojet engines are dis...
As part of a general program to study combustion in the engine cylinder and to correlate the phenome...
Conducting full-scale experiments as part of the design process of jet engine combustors is a costly...
Some of the systematic research conducted by the NACA on aircraft gas-turbine combustors is reviewed...
Research to develop high-speed airbreathing aerospace propulsion systems was underway in the late 19...
The results of an analytical investigation of the theoretical air specific impulse performance and a...