Add to ORKGThe application of large turbofan engine technology to small general aviation turbofan engines to achieve low noise, low emissions, and acceptable fuel consumption is described
The effects of advanced propellers (propfan) on aircraft direct operating costs, fuel consumption, a...
A series of iterative combustor pressure rig tests were conducted on two combustor concepts applied ...
Advanced emission reduction techniques for five existing aircraft gas turbine engines are evaluated....
NASA Lewis Research Center is conducting a program to demonstrate that large commercial engine techn...
The suitability of large engine technology to reduce noise, emissions, and fuel consumption of small...
The preliminary design of an engine which satisfies the requirements of a quiet, clean, general avia...
A model TFE731-1 engine was used as a baseline for the NASA quiet clean general aviation turbofan en...
A series of Model TFE731-2 engine tests were conducted with the Concept 2 variable geometry airblast...
The preliminary design of the over-the-wing flight propulsion system installation and nacelle compon...
The QCSEE Program provides for the design, fabrication, and testing of two experimental high-bypass ...
In an effort to increase fuel efficiency and reduce noise in commercial airplanes, NASA aeronautics ...
The NASA Environmentally Responsible Aviation (ERA) program is maturing technologies to enable simul...
The research objectives of the NASA aircraft energy efficiency program are summarized. Engine compon...
A series of combustor pressure rig screening tests was conducted on three combustor concepts applied...
A digital electronic control was combined with conventional hydromechanical components to operate th...
The effects of advanced propellers (propfan) on aircraft direct operating costs, fuel consumption, a...
A series of iterative combustor pressure rig tests were conducted on two combustor concepts applied ...
Advanced emission reduction techniques for five existing aircraft gas turbine engines are evaluated....
NASA Lewis Research Center is conducting a program to demonstrate that large commercial engine techn...
The suitability of large engine technology to reduce noise, emissions, and fuel consumption of small...
The preliminary design of an engine which satisfies the requirements of a quiet, clean, general avia...
A model TFE731-1 engine was used as a baseline for the NASA quiet clean general aviation turbofan en...
A series of Model TFE731-2 engine tests were conducted with the Concept 2 variable geometry airblast...
The preliminary design of the over-the-wing flight propulsion system installation and nacelle compon...
The QCSEE Program provides for the design, fabrication, and testing of two experimental high-bypass ...
In an effort to increase fuel efficiency and reduce noise in commercial airplanes, NASA aeronautics ...
The NASA Environmentally Responsible Aviation (ERA) program is maturing technologies to enable simul...
The research objectives of the NASA aircraft energy efficiency program are summarized. Engine compon...
A series of combustor pressure rig screening tests was conducted on three combustor concepts applied...
A digital electronic control was combined with conventional hydromechanical components to operate th...
The effects of advanced propellers (propfan) on aircraft direct operating costs, fuel consumption, a...
A series of iterative combustor pressure rig tests were conducted on two combustor concepts applied ...
Advanced emission reduction techniques for five existing aircraft gas turbine engines are evaluated....