Add to ORKGA cooperative government-industry effort, the Energy Efficient Engine Project, to develop the advanced technology base for future commercial development of a new generation of more fuel conservative turbofan engines for airline use is described. Engine configurations that are dependent upon technology advances in each major engine component are defined and current design and development of the advanced components are included
The Engine Component Improvement (ECI) Project formulated to address near term improvements for curr...
Significant advances in high bypass turbofan technologies that enhance fuel efficiency have been dem...
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...
The Energy Efficient Engine Project is directed at providing, by 1984, the advanced technologies whi...
The status of NASA's Energy Efficient Engine Project, a comparative government-industry effort aimed...
The three engine programs that constitute the propulsion portion of NASA's Aircraft Energy Efficienc...
A brief review of the current NASA Energy Efficient Engine (E(3)) Project is presented. Included in ...
Technology for fuel-efficient subsonic CTOL transport aircraft is discussed. The engine component im...
The research objectives of the NASA aircraft energy efficiency program are summarized. Engine compon...
Parametric design and mission evaluations of advanced turbofan configurations were conducted for fut...
The Benefit/Cost Study portion of the NASA-sponsored Energy Efficient Engine Component Development a...
The near-term technology improvements which can reduce the fuel consumed in the JT9D, JT8D, and JT3D...
The efficiency of high-speed turboprop propulsion systems is considered with emphasis on fuel saving...
Technology for achieving lower installed fuel consumption and lower operating costs in future commer...
An advanced technology program is described for reduced fuel consumption in air transport. Cost bene...
The Engine Component Improvement (ECI) Project formulated to address near term improvements for curr...
Significant advances in high bypass turbofan technologies that enhance fuel efficiency have been dem...
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...
The Energy Efficient Engine Project is directed at providing, by 1984, the advanced technologies whi...
The status of NASA's Energy Efficient Engine Project, a comparative government-industry effort aimed...
The three engine programs that constitute the propulsion portion of NASA's Aircraft Energy Efficienc...
A brief review of the current NASA Energy Efficient Engine (E(3)) Project is presented. Included in ...
Technology for fuel-efficient subsonic CTOL transport aircraft is discussed. The engine component im...
The research objectives of the NASA aircraft energy efficiency program are summarized. Engine compon...
Parametric design and mission evaluations of advanced turbofan configurations were conducted for fut...
The Benefit/Cost Study portion of the NASA-sponsored Energy Efficient Engine Component Development a...
The near-term technology improvements which can reduce the fuel consumed in the JT9D, JT8D, and JT3D...
The efficiency of high-speed turboprop propulsion systems is considered with emphasis on fuel saving...
Technology for achieving lower installed fuel consumption and lower operating costs in future commer...
An advanced technology program is described for reduced fuel consumption in air transport. Cost bene...
The Engine Component Improvement (ECI) Project formulated to address near term improvements for curr...
Significant advances in high bypass turbofan technologies that enhance fuel efficiency have been dem...
Propulsion system characteristics for a long range, high subsonic (Mach 0.90 - 0.98), jet commercial...