The suitability of large engine technology to reduce noise, emissions, and fuel consumption of small turbine engines and develop new technology where required is determined. The design, fabrication, assembly, test, and delivery of the experimental engines to NASA are discussed
Acoustic treatment designs for the quiet clean short-haul experimental engines are defined. The proc...
The acoustic investigation and evaluation of the C propulsion turbofan engine are discussed. The eng...
The QCSEE Program provides for the design, fabrication, and testing of two experimental high-bypass ...
NASA Lewis Research Center is conducting a program to demonstrate that large commercial engine techn...
The experimental and flight propulsion systems are presented. The following areas are discussed: eng...
The preliminary design of an engine which satisfies the requirements of a quiet, clean, general avia...
The application of large turbofan engine technology to small general aviation turbofan engines to ac...
Efforts to develop an engine noise reduction technology suitable for use on subsonic and conventiona...
Design considerations for integration of turbofan engine with reduced noise output in jet aircraf
The QCSEE (Quiet, Clean, Short-Haul Experimental Engine) program has entered the engine test phase. ...
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...
NASA's previous Advanced Subsonic Technology (AST) Noise Reduction Program delivered the initial tec...
Engine defined with noise reduced from level of current commercial aircraft powerplant
The design, fabrication, and testing of two experimental high bypass geared turbofan engines and pro...
Acoustic treatment designs for the quiet clean short-haul experimental engines are defined. The proc...
The acoustic investigation and evaluation of the C propulsion turbofan engine are discussed. The eng...
The QCSEE Program provides for the design, fabrication, and testing of two experimental high-bypass ...
NASA Lewis Research Center is conducting a program to demonstrate that large commercial engine techn...
The experimental and flight propulsion systems are presented. The following areas are discussed: eng...
The preliminary design of an engine which satisfies the requirements of a quiet, clean, general avia...
The application of large turbofan engine technology to small general aviation turbofan engines to ac...
Efforts to develop an engine noise reduction technology suitable for use on subsonic and conventiona...
Design considerations for integration of turbofan engine with reduced noise output in jet aircraf
The QCSEE (Quiet, Clean, Short-Haul Experimental Engine) program has entered the engine test phase. ...
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...
NASA's previous Advanced Subsonic Technology (AST) Noise Reduction Program delivered the initial tec...
Engine defined with noise reduced from level of current commercial aircraft powerplant
The design, fabrication, and testing of two experimental high bypass geared turbofan engines and pro...
Acoustic treatment designs for the quiet clean short-haul experimental engines are defined. The proc...
The acoustic investigation and evaluation of the C propulsion turbofan engine are discussed. The eng...
The QCSEE Program provides for the design, fabrication, and testing of two experimental high-bypass ...