The upgraded engine as built to the original design was deficient in power and had excessive specific fuel consumption. A high instrumented version of the engine was tested to identify the sources of the engine problems. Analysis of the data shows the major problems to be low compressor and power turbine efficiency and excessive interstage duct losses. In addition, high HC and CO emission were measured at idle, and high NOx emissions at high energy speeds
The results of a test program to retrofit a high performance fixed ratio Nasvytis Multiroller Tracti...
NASA Lewis Research Center's new, world-class, 60-atm combustor research facility, the Advanced Subs...
Ranges in design and off-design operating conditions of an advanced gas turbine and their effects on...
Results are presented for the design and development of an upgraded engine. The design incorporated ...
The performance sensitivity of a two-shaft automotive gas turbine engine to changes in component per...
Fuel economy potentials were calculated and compared among ten turbomachinery configurations. All ga...
A 74.5 kW(100 hp) advanced automotive gas turbine engine is described. A design iteration to improve...
The aerodynamic performance of the inlet manifold and stator assembly of the compressor drive turbin...
Automobile gas turbine engine regenerator performance was studied in a regenerator test facility tha...
Technical work on the design and effort leading to the testing of a 74.5 kW (100 hp) automotive gas ...
In support of the Fundamental Aeronautics Program, Subsonic Rotary Wing Project, further gas turbine...
The aerodynamic performance of a redesigned compressor drive turbine of the gas turbine engine is de...
A 1 kW single cylinder free piston Stirling engine, configured as a research engine, was tested with...
Exhaust concentrations of total unburned hydrocarbons, carbon monoxide, and nitric oxide were measur...
The Chrysler/ERDA baseline automotive gas turbine engine was used to experimentally determine the po...
The results of a test program to retrofit a high performance fixed ratio Nasvytis Multiroller Tracti...
NASA Lewis Research Center's new, world-class, 60-atm combustor research facility, the Advanced Subs...
Ranges in design and off-design operating conditions of an advanced gas turbine and their effects on...
Results are presented for the design and development of an upgraded engine. The design incorporated ...
The performance sensitivity of a two-shaft automotive gas turbine engine to changes in component per...
Fuel economy potentials were calculated and compared among ten turbomachinery configurations. All ga...
A 74.5 kW(100 hp) advanced automotive gas turbine engine is described. A design iteration to improve...
The aerodynamic performance of the inlet manifold and stator assembly of the compressor drive turbin...
Automobile gas turbine engine regenerator performance was studied in a regenerator test facility tha...
Technical work on the design and effort leading to the testing of a 74.5 kW (100 hp) automotive gas ...
In support of the Fundamental Aeronautics Program, Subsonic Rotary Wing Project, further gas turbine...
The aerodynamic performance of a redesigned compressor drive turbine of the gas turbine engine is de...
A 1 kW single cylinder free piston Stirling engine, configured as a research engine, was tested with...
Exhaust concentrations of total unburned hydrocarbons, carbon monoxide, and nitric oxide were measur...
The Chrysler/ERDA baseline automotive gas turbine engine was used to experimentally determine the po...
The results of a test program to retrofit a high performance fixed ratio Nasvytis Multiroller Tracti...
NASA Lewis Research Center's new, world-class, 60-atm combustor research facility, the Advanced Subs...
Ranges in design and off-design operating conditions of an advanced gas turbine and their effects on...