Add to ORKGEffect of high altitude on performance & operating characteristics of turbojet engines with hydrogen and jp-4 fuel
An analytical study has been conducted to evaluate the potential endurance of remotely piloted, low ...
The acceptability of alternate fuels for future commercial transport aircraft are discussed. Using b...
Shrouded fuel injector for low pressure hydrogen combustion in high-altitude ramjet engin
Two current turbojet engines were operated with gaseous-hydrogen and JP-4 fuels at very high altitud...
Two current turbojet engines were operated with gaseous-hydrogen and JP-4 fuels at very high altitud...
Combustion efficiency of gaseous hydrogen fuel for ramjets at very high altitudes and high distortio
This analysis investigates the application of gas turbine engines at a cruise Mach number of 4
The performance of MIL-F-5624A fuels, grades JP-3 and JP-4, was investigated in an axial-flow turboj...
Effect of high altitude on performance & operating characteristics of turbojet engines with hydrogen...
Performance characteristics of four hydrocarbon fuels having high Btu per gallon were determined in ...
An investigation was conducted with a single combustor from a J47 turbojet engine using weathered av...
Performance characteristics at simulated high altitudes of prevaporizing annular turbojet combustor ...
Liquid hydrogen used as heat sink for turbine cooling in high temperature turbojet engin
Issues and techniques relative to the adaptation of aircraft engines to high altitude flight are dis...
Combustion performance characteristics of gaseous hydrogen fuel in single tubular turbojet combusto
An analytical study has been conducted to evaluate the potential endurance of remotely piloted, low ...
The acceptability of alternate fuels for future commercial transport aircraft are discussed. Using b...
Shrouded fuel injector for low pressure hydrogen combustion in high-altitude ramjet engin
Two current turbojet engines were operated with gaseous-hydrogen and JP-4 fuels at very high altitud...
Two current turbojet engines were operated with gaseous-hydrogen and JP-4 fuels at very high altitud...
Combustion efficiency of gaseous hydrogen fuel for ramjets at very high altitudes and high distortio
This analysis investigates the application of gas turbine engines at a cruise Mach number of 4
The performance of MIL-F-5624A fuels, grades JP-3 and JP-4, was investigated in an axial-flow turboj...
Effect of high altitude on performance & operating characteristics of turbojet engines with hydrogen...
Performance characteristics of four hydrocarbon fuels having high Btu per gallon were determined in ...
An investigation was conducted with a single combustor from a J47 turbojet engine using weathered av...
Performance characteristics at simulated high altitudes of prevaporizing annular turbojet combustor ...
Liquid hydrogen used as heat sink for turbine cooling in high temperature turbojet engin
Issues and techniques relative to the adaptation of aircraft engines to high altitude flight are dis...
Combustion performance characteristics of gaseous hydrogen fuel in single tubular turbojet combusto
An analytical study has been conducted to evaluate the potential endurance of remotely piloted, low ...
The acceptability of alternate fuels for future commercial transport aircraft are discussed. Using b...
Shrouded fuel injector for low pressure hydrogen combustion in high-altitude ramjet engin