A series of convergent rectangular nozzles of aspect ratios 2:1, 4:1, and 8:1 were constructed with uniform exit velocity profiles. Additional nozzles were constructed that extended the wide lip on one side of these nozzles to form beveled nozzles. Far-field acoustic measurements were made and analyzed, and the results presented. The impact of aspect ratio on jet noise was similar to that of enhanced mixing devices: reduction in aft, peak frequency noise with an increase in broadside, high frequency noise. Azimuthally, it was found that rectangular jets produced more noise directed away from their wide sides than from their narrow sides. The azimuthal dependence decreased at aft angles where noise decreased. The effect of temperature, keepi...
Experimental investigations have been carried out on beveled and asymmetric chevron nozzles to asses...
The research performed began during Spring 1991 as a project to assess the noise reduction potential...
Far field noise data were taken for convergent nozzles of various shapes and sizes at subsonic veloc...
A series of convergent rectangular nozzles of aspect ratios 2:1, 4:1, and 8:1 were constructed with ...
This paper covers far-field acoustic measurements of a family of rectangular nozzles with aspect rat...
This paper covers particle image velocimetry measurements of a family of rectangular nozzles with as...
The influence of nozzle exit geometry on jet mixing and noise production was studied experimentally ...
A family of high aspect ratio nozzles were designed to provide a parametric database of canonical em...
AbstractModern military aircraft jet engines are designed with variable-geometry nozzles to provide ...
Two embodiments of a rectangular nozzle on an aft deck are compared. In one embodiment the lower lip...
Two methods of mixing noise modification were studied for supersonic jets flowing from rectangular n...
Jet noise is a crucial component in the entire mix of aircraft-relevant noise sources. A quiet aircr...
December 1971Includes bibliographical references (leaves 39-40)The purpose of this work is to study ...
This Phase II project validated a state-of-the-art LES model, coupled with a Ffowcs Williams-Hawking...
High speed exhaust noise reduction continues to be a research challenge for supersonic cruise busine...
Experimental investigations have been carried out on beveled and asymmetric chevron nozzles to asses...
The research performed began during Spring 1991 as a project to assess the noise reduction potential...
Far field noise data were taken for convergent nozzles of various shapes and sizes at subsonic veloc...
A series of convergent rectangular nozzles of aspect ratios 2:1, 4:1, and 8:1 were constructed with ...
This paper covers far-field acoustic measurements of a family of rectangular nozzles with aspect rat...
This paper covers particle image velocimetry measurements of a family of rectangular nozzles with as...
The influence of nozzle exit geometry on jet mixing and noise production was studied experimentally ...
A family of high aspect ratio nozzles were designed to provide a parametric database of canonical em...
AbstractModern military aircraft jet engines are designed with variable-geometry nozzles to provide ...
Two embodiments of a rectangular nozzle on an aft deck are compared. In one embodiment the lower lip...
Two methods of mixing noise modification were studied for supersonic jets flowing from rectangular n...
Jet noise is a crucial component in the entire mix of aircraft-relevant noise sources. A quiet aircr...
December 1971Includes bibliographical references (leaves 39-40)The purpose of this work is to study ...
This Phase II project validated a state-of-the-art LES model, coupled with a Ffowcs Williams-Hawking...
High speed exhaust noise reduction continues to be a research challenge for supersonic cruise busine...
Experimental investigations have been carried out on beveled and asymmetric chevron nozzles to asses...
The research performed began during Spring 1991 as a project to assess the noise reduction potential...
Far field noise data were taken for convergent nozzles of various shapes and sizes at subsonic veloc...