Add to ORKGA comparison of experiment with theory is made for air ejectors having cylindrical mixing sections and operating under conditions of supersonic primary flow and either mixed or supersonic regimes of mixing. The effect on ejector performance of such parameters as mixer length and cross section, terminating diffuser, primary Mach number, and primary nozzle position is presented in terms of mass flow and pressure ratio
We use the rectangular gaseous supersonic ejector as a platform to study the mixing characteristics ...
This report shows that by applying both energy and impulse theorems the optimum throat dimension of ...
A calculating method is developed to analyze optimum performance of supersonic ejectors under the as...
A supersonic ejector is used to pump a secondary gas using a supersonic primary gas flow by augmenta...
Thrust and pumping characteristics of ejector-type exhaust nozzles at subsonic and supersonic speeds
This work aims at investigating the primary nozzle position in a proposed supersonic air ejector dev...
A low area ratio rectangular supersonic gaseous ejector is subjected to parametric evaluation to cal...
This paper deals with numerical and experimental investigation of the flow in an air to air superson...
Tests were made at a mean inlet Mach number of 0.2 with area suction applied to conical diffusers wi...
In considering propulsion systems for future supersonic civil transport, it is important to consider...
Ejectors have many applications in aerospace and energy conversion technologies. An ejector is a pas...
The article deals with pneumatic and hot wire anemometry measurement on subsonic axi-symmetric air e...
A simple, incompressible flow, ejector model was formulated and analysed. It was found that the resu...
The article deals with numerical investigation of axisymmetric subsonic air to air ejector. An analy...
We use the rectangular gaseous supersonic ejector as a platform to study the mixing characteristics ...
This report shows that by applying both energy and impulse theorems the optimum throat dimension of ...
A calculating method is developed to analyze optimum performance of supersonic ejectors under the as...
A supersonic ejector is used to pump a secondary gas using a supersonic primary gas flow by augmenta...
Thrust and pumping characteristics of ejector-type exhaust nozzles at subsonic and supersonic speeds
This work aims at investigating the primary nozzle position in a proposed supersonic air ejector dev...
A low area ratio rectangular supersonic gaseous ejector is subjected to parametric evaluation to cal...
This paper deals with numerical and experimental investigation of the flow in an air to air superson...
Tests were made at a mean inlet Mach number of 0.2 with area suction applied to conical diffusers wi...
In considering propulsion systems for future supersonic civil transport, it is important to consider...
Ejectors have many applications in aerospace and energy conversion technologies. An ejector is a pas...
The article deals with pneumatic and hot wire anemometry measurement on subsonic axi-symmetric air e...
A simple, incompressible flow, ejector model was formulated and analysed. It was found that the resu...
The article deals with numerical investigation of axisymmetric subsonic air to air ejector. An analy...
We use the rectangular gaseous supersonic ejector as a platform to study the mixing characteristics ...
This report shows that by applying both energy and impulse theorems the optimum throat dimension of ...
A calculating method is developed to analyze optimum performance of supersonic ejectors under the as...