This paper presents the effects of several mixing enhancement devices on turbulence in jet nozzles. The topics include: 1) The Advanced Subsonic Technology (AST) Program; 2) Test Programs SFNT97 and SFNT2K; 3) Facility; 4) Mixing Enhancement Nozzles; 5) IR reductions; 6) Schlieren of Chevrons; and 7) Aeroacoustics of Enhanced Mixing-Paradigm. This paper is presented in viewgraph form
A study of noise benefit, vis-a-vis thrust penalty, and its correlation to turbulence intensities wa...
The original publication can be found at www.springerlink.comExperimental results of the mixing char...
This report describes the work performed by General Electric Aircraft Engines (GEAE) and Allison Eng...
Comparison of turbulence data taken in three separate flow nozzles, two with mixing enhancement feat...
The idea of using mixing enhancement to reduce jet noise is not new. Lobed mixers have been around s...
A major contributor to the overall noise of an aircraft is jet noise – the noise generated by the ga...
As part of the Advanced Subsonic Technology Program, a series of experiments was conducted at NASA G...
Turbulent mixing enhancement of two confined, co-axial jets having a low annular to core area ratio ...
One major concern regarding supersonic jets, particularly in its application to commercial aircraft,...
Typical installed separate-flow exhaust nozzle system. The jet noise from modern turbofan engines is...
A mixing layer is a common model used to study the noise generation and mixing characteristics of th...
A numerical study employing a simplified model of the High Speed Civil Transport mixer/ejector nozzl...
The influence of modifying a jet's exit flow pattern on both the near and far-field turbulent mixing...
Turbulent mixing enhancement has received a great deal of attention in the fluid mechanics community...
The notched nozzle as a new concept has been investigated for conventional nozzle design together wi...
A study of noise benefit, vis-a-vis thrust penalty, and its correlation to turbulence intensities wa...
The original publication can be found at www.springerlink.comExperimental results of the mixing char...
This report describes the work performed by General Electric Aircraft Engines (GEAE) and Allison Eng...
Comparison of turbulence data taken in three separate flow nozzles, two with mixing enhancement feat...
The idea of using mixing enhancement to reduce jet noise is not new. Lobed mixers have been around s...
A major contributor to the overall noise of an aircraft is jet noise – the noise generated by the ga...
As part of the Advanced Subsonic Technology Program, a series of experiments was conducted at NASA G...
Turbulent mixing enhancement of two confined, co-axial jets having a low annular to core area ratio ...
One major concern regarding supersonic jets, particularly in its application to commercial aircraft,...
Typical installed separate-flow exhaust nozzle system. The jet noise from modern turbofan engines is...
A mixing layer is a common model used to study the noise generation and mixing characteristics of th...
A numerical study employing a simplified model of the High Speed Civil Transport mixer/ejector nozzl...
The influence of modifying a jet's exit flow pattern on both the near and far-field turbulent mixing...
Turbulent mixing enhancement has received a great deal of attention in the fluid mechanics community...
The notched nozzle as a new concept has been investigated for conventional nozzle design together wi...
A study of noise benefit, vis-a-vis thrust penalty, and its correlation to turbulence intensities wa...
The original publication can be found at www.springerlink.comExperimental results of the mixing char...
This report describes the work performed by General Electric Aircraft Engines (GEAE) and Allison Eng...