Add to ORKGPerformance tests and characteristics of short length, double annular ram induction turbojet combustion chambers for supersonic fligh
Free jet tests of 48 inch diameter ramjet combustor with annular can-type flame holde
Annular diffuser and combustor assembly in full scale duct burner for supersonic turbofan engin
Two short turbojet combustors designed for use with vaporized hydrocarbon fuels were tested in a one...
Full-scale annular ram-induction combustor tests for Mach 3 cruise turbojet engin
A performance development program has been conducted on a short length, double-annular, ram-inductio...
Performance tests of short length, gas turbine combustors with atomized or vaporized fuel injectio
Short length combustor and diffuser configuration for supersonic cruise turbofan engin
Separate component test rigs for 90 degree sector combustor and full annular turbojet combustor comp...
The report describes the design of a piloted combustor intended for a ram-jet engine of long flight ...
Evaluating performance of swirl can turbojet combustor at simulated supersonic inlet condition
An extensive test program was undertaken to determine the effect of many design features such as the...
A test program was conducted to evaluate an experimental short-length annular combustor that uses a ...
Performance tests of rectangular sector of turbojet combustor consisting of array of modul
Hydrogen burning annular combustor in miniature gas turbine engine for wind tunnel tests for obtaini...
A full scale double-annular ram-induction combustor designed for Mach 3.0 cruise operation was teste...
Free jet tests of 48 inch diameter ramjet combustor with annular can-type flame holde
Annular diffuser and combustor assembly in full scale duct burner for supersonic turbofan engin
Two short turbojet combustors designed for use with vaporized hydrocarbon fuels were tested in a one...
Full-scale annular ram-induction combustor tests for Mach 3 cruise turbojet engin
A performance development program has been conducted on a short length, double-annular, ram-inductio...
Performance tests of short length, gas turbine combustors with atomized or vaporized fuel injectio
Short length combustor and diffuser configuration for supersonic cruise turbofan engin
Separate component test rigs for 90 degree sector combustor and full annular turbojet combustor comp...
The report describes the design of a piloted combustor intended for a ram-jet engine of long flight ...
Evaluating performance of swirl can turbojet combustor at simulated supersonic inlet condition
An extensive test program was undertaken to determine the effect of many design features such as the...
A test program was conducted to evaluate an experimental short-length annular combustor that uses a ...
Performance tests of rectangular sector of turbojet combustor consisting of array of modul
Hydrogen burning annular combustor in miniature gas turbine engine for wind tunnel tests for obtaini...
A full scale double-annular ram-induction combustor designed for Mach 3.0 cruise operation was teste...
Free jet tests of 48 inch diameter ramjet combustor with annular can-type flame holde
Annular diffuser and combustor assembly in full scale duct burner for supersonic turbofan engin
Two short turbojet combustors designed for use with vaporized hydrocarbon fuels were tested in a one...