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...
The ram jet is basically one of the most dimple types of aircraft engine. It consists only of an inl...
DVL experimental and analytical work on the cooling of turbine blades by using ram air as the workin...
Theoretical studies of the turbojet and ramjet combustion process are summarized and the resulting e...
The report summarizes source material on combustion for flight-propulsion engineers. First, several ...
Convenient charts are presented for computing the thrust, fuel consumption, and other performance va...
An investigation was conducted t o determine the hrgortance of molecular-scale processes in the over...
The combustion performance, and particularly the phenomenon of altitude operational limits, was stud...
Based on the assumption that shock-free internal burning is possible in a supersonic airstream, calc...
Following a brief history of the NACA investigation of jet-propulsion, a discussion is given of the ...
The development and the use of a chart for use in estimating the combustion efficiency of a turbojet...
The combustion performance and particularly the phenomenon of altitude operational limits was studie...
NACA research on the single problem of combustion efficiency of turbojet engines at high altitudes i...
NACA research on afterburners for turbojet engines during the past 5 years is summarized. Although m...
Some of the systematic research conducted by the NACA on aircraft gas-turbine combustors is reviewed...
The ram jet is basically one of the most dimple types of aircraft engine. It consists only of an inl...
DVL experimental and analytical work on the cooling of turbine blades by using ram air as the workin...
Theoretical studies of the turbojet and ramjet combustion process are summarized and the resulting e...
The report summarizes source material on combustion for flight-propulsion engineers. First, several ...
Convenient charts are presented for computing the thrust, fuel consumption, and other performance va...
An investigation was conducted t o determine the hrgortance of molecular-scale processes in the over...
The combustion performance, and particularly the phenomenon of altitude operational limits, was stud...
Based on the assumption that shock-free internal burning is possible in a supersonic airstream, calc...
Following a brief history of the NACA investigation of jet-propulsion, a discussion is given of the ...
The development and the use of a chart for use in estimating the combustion efficiency of a turbojet...
The combustion performance and particularly the phenomenon of altitude operational limits was studie...
NACA research on the single problem of combustion efficiency of turbojet engines at high altitudes i...
NACA research on afterburners for turbojet engines during the past 5 years is summarized. Although m...
Some of the systematic research conducted by the NACA on aircraft gas-turbine combustors is reviewed...
The ram jet is basically one of the most dimple types of aircraft engine. It consists only of an inl...
DVL experimental and analytical work on the cooling of turbine blades by using ram air as the workin...