This paper covers particle image velocimetry measurements of a family of rectangular nozzles with aspect ratios 2, 4, and 8, in the high subsonic flow regime. Far-field acoustic results, presented previously, showed that increasing aspect ratios increased the high frequency noise, especially directed in the polar plane containing the minor axis of the nozzle. The measurements presented here have important implications in the modeling of turbulent sources for acoustic analogy theories. While the nonaxisymmetric mean flow from the rectangular nozzles can be studied reliably using computational solutions, the nonaxisymmetry of the turbulent fluctuations, particularly at the level of velocity components, cannot; only measurements such as these ...
Direct numerical simulations (DNS) of the full-scale rectangular nozzle of a hypersonic wind tunnel ...
An experimental and computational fluid dynamics study is reported of supersonic jets issuing from a...
As part of the Advanced Subsonic Technology Program, a series of experiments was conducted at NASA G...
A series of convergent rectangular nozzles of aspect ratios 2:1, 4:1, and 8:1 were constructed with ...
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 far-field acoustic measurements of a family of rectangular nozzles with aspect rat...
A family of high aspect ratio nozzles were designed to provide a parametric database of canonical em...
The influence of nozzle exit geometry on jet mixing and noise production was studied experimentally ...
AbstractModern military aircraft jet engines are designed with variable-geometry nozzles to provide ...
Turbulent free jets issuing from rectangular slots with various high aspect ratios (15-120) are char...
Supersonic flight has become a standard for military aircraft, and is being seriously reconsidered f...
An experimental study is reported of underexpanded supersonic jet plumes issuing from a high-aspect-...
University of Minnesota M.S. thesis. June 2015. Major: Aerospace Engineering and Mechanics. Advisor:...
Two embodiments of a rectangular nozzle on an aft deck are compared. In one embodiment the lower lip...
Direct numerical simulations (DNS) of the full-scale rectangular nozzle of a hypersonic wind tunnel ...
An experimental and computational fluid dynamics study is reported of supersonic jets issuing from a...
As part of the Advanced Subsonic Technology Program, a series of experiments was conducted at NASA G...
A series of convergent rectangular nozzles of aspect ratios 2:1, 4:1, and 8:1 were constructed with ...
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 far-field acoustic measurements of a family of rectangular nozzles with aspect rat...
A family of high aspect ratio nozzles were designed to provide a parametric database of canonical em...
The influence of nozzle exit geometry on jet mixing and noise production was studied experimentally ...
AbstractModern military aircraft jet engines are designed with variable-geometry nozzles to provide ...
Turbulent free jets issuing from rectangular slots with various high aspect ratios (15-120) are char...
Supersonic flight has become a standard for military aircraft, and is being seriously reconsidered f...
An experimental study is reported of underexpanded supersonic jet plumes issuing from a high-aspect-...
University of Minnesota M.S. thesis. June 2015. Major: Aerospace Engineering and Mechanics. Advisor:...
Two embodiments of a rectangular nozzle on an aft deck are compared. In one embodiment the lower lip...
Direct numerical simulations (DNS) of the full-scale rectangular nozzle of a hypersonic wind tunnel ...
An experimental and computational fluid dynamics study is reported of supersonic jets issuing from a...
As part of the Advanced Subsonic Technology Program, a series of experiments was conducted at NASA G...