Noise measurements were taken on a turbofan engine which uses the same core, with minor modifications, employed on the quiet clean short-haul experimental engine (QCSEE) propulsion systems. Both nearfield and farfield noise measurements were taken in order to determine the core internally generated noise levels. The resulting noise measurements were compared to predicted combustor and turbine noise levels, to verify or improve the predicted QCSEE combustor and turbine noise levels
As part of a program to investigate combustor and other core noises, simultaneous measurements of in...
A component pressure test was conducted on a F101 PFRT combustor to evaluate the emissions levels of...
Acoustical tests of full scale fans for jet engines are presented. The fans are described and some a...
Core noise from a YF-102 high bypass ratio turbofan engine was investigated through the use of simul...
Acoustic treatment designs for the quiet clean short-haul experimental engines are defined. The proc...
A series of acoustic tests were conducted on the over the wing engine. These tests evaluated the ful...
The core noise levels from gas turbine aircraft engines were measured using a technique which requir...
The experimental and flight propulsion systems are presented. The following areas are discussed: eng...
The acoustic investigation and evaluation of the C propulsion turbofan engine are discussed. The eng...
A quiet, clean, general aviation, turbofan engine was instrumented to measure the fluctuating pressu...
The AiResearch Quiet Clean General Aviation Turbofan engine was tested on an outdoor test stand to c...
The suitability of large engine technology to reduce noise, emissions, and fuel consumption of small...
The contribution of the standard production annular combustor to the far-field noise signature of th...
The acoustic considerations involved in the low source noise basic engine design and the design proc...
The acoustic considerations involved in the low source noise basic engine design and the design proc...
As part of a program to investigate combustor and other core noises, simultaneous measurements of in...
A component pressure test was conducted on a F101 PFRT combustor to evaluate the emissions levels of...
Acoustical tests of full scale fans for jet engines are presented. The fans are described and some a...
Core noise from a YF-102 high bypass ratio turbofan engine was investigated through the use of simul...
Acoustic treatment designs for the quiet clean short-haul experimental engines are defined. The proc...
A series of acoustic tests were conducted on the over the wing engine. These tests evaluated the ful...
The core noise levels from gas turbine aircraft engines were measured using a technique which requir...
The experimental and flight propulsion systems are presented. The following areas are discussed: eng...
The acoustic investigation and evaluation of the C propulsion turbofan engine are discussed. The eng...
A quiet, clean, general aviation, turbofan engine was instrumented to measure the fluctuating pressu...
The AiResearch Quiet Clean General Aviation Turbofan engine was tested on an outdoor test stand to c...
The suitability of large engine technology to reduce noise, emissions, and fuel consumption of small...
The contribution of the standard production annular combustor to the far-field noise signature of th...
The acoustic considerations involved in the low source noise basic engine design and the design proc...
The acoustic considerations involved in the low source noise basic engine design and the design proc...
As part of a program to investigate combustor and other core noises, simultaneous measurements of in...
A component pressure test was conducted on a F101 PFRT combustor to evaluate the emissions levels of...
Acoustical tests of full scale fans for jet engines are presented. The fans are described and some a...