A theoretical analysis of the viscous interaction between the primary and secondary streams of ejector nozzles was developed. The analysis accounts for real sonic line effects and the streamwise variation in stream mixing and boundary layer within the ejector. The aspects of the analysis are explained and illustrated by applying the theory to a variety of ejector configurations including cylindrical shroud, contoured flap and plug nozzles. Extensive comparisons are made between theory and data to show the importance of various analytical assumptions and such design variables as diameter ratio, spacing ratio, total temperature ratio, and primary nozzle geometry
Experimental results from a wind tunnel test conducted to investigate propulsion/airframe integratio...
Different applications of a variable area convergent-divergent nozzle are found in various parts of ...
A three-dimensional full Navier-Stokes (FNS) analysis was performed on a mixer/ejector nozzle design...
An analytical procedure for computing the performance of supersonic ejector nozzles is presented. Th...
The ability of analysis to predict ejector nozzle characteristics over a wide range of conditions an...
The effect of initial velocity profile on the performance of axisymmetric supersonic ejector nozzles...
A time-iterative full Navier-Stokes code, PARC, is used to analyze the flowfield of a two-dimensiona...
A fundamental exploratory experiment is conducted assessing the performance of a one-sided ejector w...
Attached primary nozzles were developed to replace the detached nozzles of jet-diffuser ejectors. Sl...
The factors affecting the performance of ejector suitable for aircraft cooling are investigated theo...
The following cold-flow study examines the interaction of the diffracted shock wave pattern and the ...
Pumping characteristics of variable geometry ejectors with hot and cold primary nozzle flo
A finite difference procedure was used to compute the mixing for three experimentally tested mixer g...
The process is discussed of designing a nozzle for a hypersonic airbreathing vehicle which involves ...
A finite difference procedure was developed to analyze the three dimensional subsonic turbulent flow...
Experimental results from a wind tunnel test conducted to investigate propulsion/airframe integratio...
Different applications of a variable area convergent-divergent nozzle are found in various parts of ...
A three-dimensional full Navier-Stokes (FNS) analysis was performed on a mixer/ejector nozzle design...
An analytical procedure for computing the performance of supersonic ejector nozzles is presented. Th...
The ability of analysis to predict ejector nozzle characteristics over a wide range of conditions an...
The effect of initial velocity profile on the performance of axisymmetric supersonic ejector nozzles...
A time-iterative full Navier-Stokes code, PARC, is used to analyze the flowfield of a two-dimensiona...
A fundamental exploratory experiment is conducted assessing the performance of a one-sided ejector w...
Attached primary nozzles were developed to replace the detached nozzles of jet-diffuser ejectors. Sl...
The factors affecting the performance of ejector suitable for aircraft cooling are investigated theo...
The following cold-flow study examines the interaction of the diffracted shock wave pattern and the ...
Pumping characteristics of variable geometry ejectors with hot and cold primary nozzle flo
A finite difference procedure was used to compute the mixing for three experimentally tested mixer g...
The process is discussed of designing a nozzle for a hypersonic airbreathing vehicle which involves ...
A finite difference procedure was developed to analyze the three dimensional subsonic turbulent flow...
Experimental results from a wind tunnel test conducted to investigate propulsion/airframe integratio...
Different applications of a variable area convergent-divergent nozzle are found in various parts of ...
A three-dimensional full Navier-Stokes (FNS) analysis was performed on a mixer/ejector nozzle design...