Add to ORKGResults of initial tests of the under the wing experimental engine and boilerplate nacelle are presented. The mechanical performance of the engine is reported with emphasis on the advanced technology components. Technology elements of the propulsion system covered include: system dynamics, composite fan blades, reduction gear, lube and accessory drive system, fan frame, inlet, core cowl cooling, fan exhaust nozzle, and digital control system
A digital electronic control was combined with conventional hydromechanical components to operate th...
The QCSEE Program provides for the design, fabrication, and testing of two experimental high-bypass ...
The element and subcomponent testing conducted to verify the composite fan frame design of two exper...
The design and testing of high bypass geared turbofan engines with nacelles forming the propulsion s...
The mechanical performance of the over-the-wing engine is described with emphasis on the advanced te...
The detail design of the under the wing experimental composite nacelle components is summarized. Ana...
Sea level, static, ground testing of the over-the-wing engine and boilerplate nacelle components was...
The initial phase of testing of the under the wing engine and boilerplate nacelle components is disc...
The mechanical design of the boiler plate nacelle and core exhaust nozzle for the QCSEE under the wi...
A summary of the mechanical design of the boiler plate nacelle for the QCSEE over the wing (OTW) eng...
The design, fabrication, and testing of two experimental high bypass geared turbofan engines and pro...
The element and subcomponent testing conducted to verify the under the wing composite nacelle design...
The experimental and flight propulsion systems are presented. The following areas are discussed: eng...
The preliminary design and installation of high bypass, geared turbofan engine with a composite nace...
The preliminary design of the over-the-wing flight propulsion system installation and nacelle compon...
A digital electronic control was combined with conventional hydromechanical components to operate th...
The QCSEE Program provides for the design, fabrication, and testing of two experimental high-bypass ...
The element and subcomponent testing conducted to verify the composite fan frame design of two exper...
The design and testing of high bypass geared turbofan engines with nacelles forming the propulsion s...
The mechanical performance of the over-the-wing engine is described with emphasis on the advanced te...
The detail design of the under the wing experimental composite nacelle components is summarized. Ana...
Sea level, static, ground testing of the over-the-wing engine and boilerplate nacelle components was...
The initial phase of testing of the under the wing engine and boilerplate nacelle components is disc...
The mechanical design of the boiler plate nacelle and core exhaust nozzle for the QCSEE under the wi...
A summary of the mechanical design of the boiler plate nacelle for the QCSEE over the wing (OTW) eng...
The design, fabrication, and testing of two experimental high bypass geared turbofan engines and pro...
The element and subcomponent testing conducted to verify the under the wing composite nacelle design...
The experimental and flight propulsion systems are presented. The following areas are discussed: eng...
The preliminary design and installation of high bypass, geared turbofan engine with a composite nace...
The preliminary design of the over-the-wing flight propulsion system installation and nacelle compon...
A digital electronic control was combined with conventional hydromechanical components to operate th...
The QCSEE Program provides for the design, fabrication, and testing of two experimental high-bypass ...
The element and subcomponent testing conducted to verify the composite fan frame design of two exper...