Add to ORKGThe aerodynamic and mechanical preliminary design of the QCSEE over the wing 1.36 pressure ratio fan is presented. Design information is given for both the experimental and flight designs
The design and testing of high bypass geared turbofan engines with nacelles forming the propulsion s...
Results of initial tests of the under the wing experimental engine and boilerplate nacelle are prese...
The mechanical design of the boiler plate nacelle and core exhaust nozzle for the QCSEE under the wi...
High bypass geared turbofan engines and propulsion systems designed for short-haul passenger aircraf...
The experimental and flight propulsion systems are presented. The following areas are discussed: eng...
The design, fabrication, and testing of two experimental high bypass geared turbofan engines and pro...
The QCSEE Program provides for the design, fabrication, and testing of two experimental high-bypass ...
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...
Results of tests conducted on preliminary design polymeric-composite fan blade for the under the win...
A static scale model test program was conducted in the static test area of the NASA-Langley 9.14- by...
The preliminary design and installation of high bypass, geared turbofan engine with a composite nace...
The aerodynamic and mechanical design of a fixed-pitch 1.36 pressure ratio fan for the over-the-wing...
The mechanical performance of the over-the-wing engine is described with emphasis on the advanced te...
A digital electronic control was combined with conventional hydromechanical components to operate th...
The design and testing of high bypass geared turbofan engines with nacelles forming the propulsion s...
Results of initial tests of the under the wing experimental engine and boilerplate nacelle are prese...
The mechanical design of the boiler plate nacelle and core exhaust nozzle for the QCSEE under the wi...
High bypass geared turbofan engines and propulsion systems designed for short-haul passenger aircraf...
The experimental and flight propulsion systems are presented. The following areas are discussed: eng...
The design, fabrication, and testing of two experimental high bypass geared turbofan engines and pro...
The QCSEE Program provides for the design, fabrication, and testing of two experimental high-bypass ...
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...
Results of tests conducted on preliminary design polymeric-composite fan blade for the under the win...
A static scale model test program was conducted in the static test area of the NASA-Langley 9.14- by...
The preliminary design and installation of high bypass, geared turbofan engine with a composite nace...
The aerodynamic and mechanical design of a fixed-pitch 1.36 pressure ratio fan for the over-the-wing...
The mechanical performance of the over-the-wing engine is described with emphasis on the advanced te...
A digital electronic control was combined with conventional hydromechanical components to operate th...
The design and testing of high bypass geared turbofan engines with nacelles forming the propulsion s...
Results of initial tests of the under the wing experimental engine and boilerplate nacelle are prese...
The mechanical design of the boiler plate nacelle and core exhaust nozzle for the QCSEE under the wi...