Add to ORKGMethods of introducing and distributing air and fuel in turbojet-engine combustors were evaluated wi...
Conversion of experimental turbojet combustor from ASTM A-1 fuel to natural gas fue
As part of a continuing effort at the Lewis Research Center to improve performance, emissions, and r...
Performance tests and characteristics of short length, double annular ram induction turbojet combust...
A performance development program has been conducted on a short length, double-annular, ram-inductio...
Short length combustor and diffuser configuration for supersonic cruise turbofan engin
Two short turbojet combustors designed for use with vaporized hydrocarbon fuels were tested in a one...
Performance tests of rectangular sector of turbojet combustor consisting of array of modul
Two short turbojet combustors designed for use with vaporized hydrocarbon fuels were tested in a one...
Hydrogen burning annular combustor in miniature gas turbine engine for wind tunnel tests for obtaini...
Full-scale annular ram-induction combustor tests for Mach 3 cruise turbojet engin
Performance investigations were conducted on a combustor utilizing several cost-reducing innovations...
A series of combustor pressure rig screening tests was conducted on three combustor concepts applied...
A test program was conducted to evaluate an experimental short-length annular combustor that uses a ...
Performance tests were conducted on a combustor designed for use in a low-cost turbojet engine. Low-...
Methods of introducing and distributing air and fuel in turbojet-engine combustors were evaluated wi...
Conversion of experimental turbojet combustor from ASTM A-1 fuel to natural gas fue
As part of a continuing effort at the Lewis Research Center to improve performance, emissions, and r...
Performance tests and characteristics of short length, double annular ram induction turbojet combust...
A performance development program has been conducted on a short length, double-annular, ram-inductio...
Short length combustor and diffuser configuration for supersonic cruise turbofan engin
Two short turbojet combustors designed for use with vaporized hydrocarbon fuels were tested in a one...
Performance tests of rectangular sector of turbojet combustor consisting of array of modul
Two short turbojet combustors designed for use with vaporized hydrocarbon fuels were tested in a one...
Hydrogen burning annular combustor in miniature gas turbine engine for wind tunnel tests for obtaini...
Full-scale annular ram-induction combustor tests for Mach 3 cruise turbojet engin
Performance investigations were conducted on a combustor utilizing several cost-reducing innovations...
A series of combustor pressure rig screening tests was conducted on three combustor concepts applied...
A test program was conducted to evaluate an experimental short-length annular combustor that uses a ...
Performance tests were conducted on a combustor designed for use in a low-cost turbojet engine. Low-...
Methods of introducing and distributing air and fuel in turbojet-engine combustors were evaluated wi...
Conversion of experimental turbojet combustor from ASTM A-1 fuel to natural gas fue
As part of a continuing effort at the Lewis Research Center to improve performance, emissions, and r...