Add to ORKGThe preliminary design and installation of high bypass, geared turbofan engine with a composite nacelle forming the propulsion system for a short haul passenger aircraft are described. The technology required for externally blown flap aircraft with under the wing (UTW) propulsion system installations for introduction into passenger service in the mid 1980's is included. The design, fabrication, and testing of this UTW experimental engine containing the required technology items for low noise, fuel economy, with composite structure for reduced weight and digital engine control are provided
The aerodynamic and mechanical preliminary design of the QCSEE over the wing 1.36 pressure ratio fan...
The mechanical performance of the over-the-wing engine is described with emphasis on the advanced te...
The mechanical design of the boiler plate nacelle and core exhaust nozzle for the QCSEE under the wi...
The design and testing of high bypass geared turbofan engines with nacelles forming the propulsion s...
The design, fabrication, and testing of two experimental high bypass geared turbofan engines and pro...
The preliminary design of the over-the-wing flight propulsion system installation and nacelle compon...
The detail design of the under the wing experimental composite nacelle components is summarized. Ana...
The QCSEE Program provides for the design, fabrication, and testing of two experimental high-bypass ...
The experimental and flight propulsion systems are presented. The following areas are discussed: eng...
High bypass geared turbofan engines and propulsion systems designed for short-haul passenger aircraf...
Sea level, static, ground testing of the over-the-wing engine and boilerplate nacelle components was...
The QCSEE (Quiet, Clean, Short-Haul Experimental Engine) program has entered the engine test phase. ...
A digital electronic control was combined with conventional hydromechanical components to operate th...
The design, fabrication, and testing of two experimental propulsion systems for powered lift transpo...
Results of initial tests of the under the wing experimental engine and boilerplate nacelle are prese...
The aerodynamic and mechanical preliminary design of the QCSEE over the wing 1.36 pressure ratio fan...
The mechanical performance of the over-the-wing engine is described with emphasis on the advanced te...
The mechanical design of the boiler plate nacelle and core exhaust nozzle for the QCSEE under the wi...
The design and testing of high bypass geared turbofan engines with nacelles forming the propulsion s...
The design, fabrication, and testing of two experimental high bypass geared turbofan engines and pro...
The preliminary design of the over-the-wing flight propulsion system installation and nacelle compon...
The detail design of the under the wing experimental composite nacelle components is summarized. Ana...
The QCSEE Program provides for the design, fabrication, and testing of two experimental high-bypass ...
The experimental and flight propulsion systems are presented. The following areas are discussed: eng...
High bypass geared turbofan engines and propulsion systems designed for short-haul passenger aircraf...
Sea level, static, ground testing of the over-the-wing engine and boilerplate nacelle components was...
The QCSEE (Quiet, Clean, Short-Haul Experimental Engine) program has entered the engine test phase. ...
A digital electronic control was combined with conventional hydromechanical components to operate th...
The design, fabrication, and testing of two experimental propulsion systems for powered lift transpo...
Results of initial tests of the under the wing experimental engine and boilerplate nacelle are prese...
The aerodynamic and mechanical preliminary design of the QCSEE over the wing 1.36 pressure ratio fan...
The mechanical performance of the over-the-wing engine is described with emphasis on the advanced te...
The mechanical design of the boiler plate nacelle and core exhaust nozzle for the QCSEE under the wi...