The effects of mechanical protrusions on the jet mixing characteristics of rectangular nozzles for heated and unheated subsonic and supersonic jet plumes were studied. The characteristics of a rectangular nozzle of aspect ratio 4 without the mechanical protrusions were first investigated. Intrusive probes were used to make the flow measurements. Possible errors introduced by intrusive probes in making shear flow measurements were also examined. Several scaled sizes of mechanical tabs were then tested, configured around the perimeter of the rectangular jet. Both the number and the location of the tabs were varied. From this, the best configuration was selected. The conclusions derived were: (1) intrusive probes can produce significant errors...
Results from an experimental investigation to study the distribution of local effectiveness and Nuss...
An experimental study is reported of underexpanded supersonic jet plumes issuing from a high-aspect-...
The effect of vortex generators, in the form of small tabs at the nozzle exit, on the evolution of a...
The effects of mechanical protrusions on the jet mixing characteristics of rectangular nozzles for h...
This effort was conducted to obtain additional test data/configurations required to better understan...
Test data is presented which allows determination of jet penetration and mixing of multiple cold air...
The objective of this study was to analyze jet plume mass flow entrainment rates associated with the...
An experimental and computational fluid dynamics study is reported of supersonic jets issuing from a...
Plasma-controlled turbulent jets are investigated by means of Implicit Large–Eddy Simulations at a R...
Study was conducted to determine penetration and mixing characteristics of multiple jets of ambient ...
Survey develops adequate heat transfer correlations for design use. Flow characteristics studies inc...
Experimental observations show that the presence of small tabs on the edge of a hot, compressible je...
December 1971Includes bibliographical references (leaves 39-40)The purpose of this work is to study ...
Flow control techniques for increasing the rate of jet mixing in axisymmetric nozzle flows have been...
It is well known that the triangular tab is an effective device to enhance jet’s mixing. However, du...
Results from an experimental investigation to study the distribution of local effectiveness and Nuss...
An experimental study is reported of underexpanded supersonic jet plumes issuing from a high-aspect-...
The effect of vortex generators, in the form of small tabs at the nozzle exit, on the evolution of a...
The effects of mechanical protrusions on the jet mixing characteristics of rectangular nozzles for h...
This effort was conducted to obtain additional test data/configurations required to better understan...
Test data is presented which allows determination of jet penetration and mixing of multiple cold air...
The objective of this study was to analyze jet plume mass flow entrainment rates associated with the...
An experimental and computational fluid dynamics study is reported of supersonic jets issuing from a...
Plasma-controlled turbulent jets are investigated by means of Implicit Large–Eddy Simulations at a R...
Study was conducted to determine penetration and mixing characteristics of multiple jets of ambient ...
Survey develops adequate heat transfer correlations for design use. Flow characteristics studies inc...
Experimental observations show that the presence of small tabs on the edge of a hot, compressible je...
December 1971Includes bibliographical references (leaves 39-40)The purpose of this work is to study ...
Flow control techniques for increasing the rate of jet mixing in axisymmetric nozzle flows have been...
It is well known that the triangular tab is an effective device to enhance jet’s mixing. However, du...
Results from an experimental investigation to study the distribution of local effectiveness and Nuss...
An experimental study is reported of underexpanded supersonic jet plumes issuing from a high-aspect-...
The effect of vortex generators, in the form of small tabs at the nozzle exit, on the evolution of a...