Add to ORKGAn investigation of a single-annulus turbojet combustor with slot-type air admission was conducted to demonstrate the application of certain design principles to the control of outlet-gas temperature distributions. Comparisons of performance of a one-quarter-annulus combustor (duct-type installation) and a full-annulus combustor (obtained in a full-scale turbojet engine) are presented to indicate the applicability of results obtained from combustion studies conducted in duct-type installations. A reasonable correlation existed between the performance of the one-quarter-annulus and full-annulus combustors except for temperature distribution. Sufficient trends did exist which made it possible to predict temperature distributions for the engin...
Temperature surveys were made at the combustion-chamber outlets of a British Rolls-Royce Nene II eng...
Compressible and incompressible flow calculations were made of the combustor total-pressure-loss coe...
A test program was conducted to evaluate an experimental short-length annular combustor that uses a ...
An investigation of a single-annulus turbojet combustor with slot-type air admission was conducted t...
"An investigation has been conducted on a one-sixth segment of an annular turbojet combustor to dete...
The combustion performance and particularly the phenomenon of altitude operational limits was studie...
The combustion performance, and particularly the phenomenon of altitude operational limits, was stud...
Methods of introducing and distributing air and fuel in turbojet-engine combustors were evaluated wi...
The combustor total-pressure-loss coefficient and liner air-flow distribution are presented graphica...
Separate component test rigs for 90 degree sector combustor and full annular turbojet combustor comp...
A number of short turbojet combustor configurations for hydrogen f u e l were designed and their per...
Some of the systematic research conducted by the NACA on aircraft gas-turbine combustors is reviewed...
The design principle of injecting liquid fuel at more than one axial station in an annual turbojet c...
The desirability of obtaining an even distribution of temperature at the outlet of a ramjet combust...
Temperature surveys were made at the combustion-chamber outlets of a British Rolls-Royce Nene II eng...
Compressible and incompressible flow calculations were made of the combustor total-pressure-loss coe...
A test program was conducted to evaluate an experimental short-length annular combustor that uses a ...
An investigation of a single-annulus turbojet combustor with slot-type air admission was conducted t...
"An investigation has been conducted on a one-sixth segment of an annular turbojet combustor to dete...
The combustion performance and particularly the phenomenon of altitude operational limits was studie...
The combustion performance, and particularly the phenomenon of altitude operational limits, was stud...
Methods of introducing and distributing air and fuel in turbojet-engine combustors were evaluated wi...
The combustor total-pressure-loss coefficient and liner air-flow distribution are presented graphica...
Separate component test rigs for 90 degree sector combustor and full annular turbojet combustor comp...
A number of short turbojet combustor configurations for hydrogen f u e l were designed and their per...
Some of the systematic research conducted by the NACA on aircraft gas-turbine combustors is reviewed...
The design principle of injecting liquid fuel at more than one axial station in an annual turbojet c...
The desirability of obtaining an even distribution of temperature at the outlet of a ramjet combust...
Temperature surveys were made at the combustion-chamber outlets of a British Rolls-Royce Nene II eng...
Compressible and incompressible flow calculations were made of the combustor total-pressure-loss coe...
A test program was conducted to evaluate an experimental short-length annular combustor that uses a ...