Add to ORKGThe effect of initial velocity profile on the performance of axisymmetric supersonic ejector nozzles is discussed. Two different initial profiles in each of two different geometries are analyzed, and the importance of using realistic starting conditions to predict supersonic nozzle performance is demonstrated
Pumping characteristics of variable geometry ejectors with hot and cold primary nozzle flo
Pumping and internal thrust performance of simulated variable divergent-shroud ejector nozzle design...
An improved ability to predict external propulsive performance was incorporated into the three-dimen...
A theoretical analysis of the viscous interaction between the primary and secondary streams of eject...
A computer program previously developed to analyze three-dimensional supersonic nozzles by the metho...
The ability of analysis to predict ejector nozzle characteristics over a wide range of conditions an...
An analytical procedure for computing the performance of supersonic ejector nozzles is presented. Th...
Flows through three reference nozzles have been calculated to determine the capabilities and limitat...
An experiment was conducted at static conditions to determine the internal performance effects of no...
This paper discusses a test of a nozzle concept for a high-speed commercial aircraft. While a great ...
An investigation was conducted in the model preparation area of the Langley 16-Foot Transonic Tunnel...
Numerous experiments were conducted to determine factors which affect the internal performance of co...
An experimental investigation of a series of four convergent-divergent exhaust nozzles was conducted...
Conventional procedures for designing nozzles involve the design of an inviscid contour (using the m...
Effects of shroud geometry on performance of collapsible plug nozzle at Mach numbers from 0 to 2.
Pumping characteristics of variable geometry ejectors with hot and cold primary nozzle flo
Pumping and internal thrust performance of simulated variable divergent-shroud ejector nozzle design...
An improved ability to predict external propulsive performance was incorporated into the three-dimen...
A theoretical analysis of the viscous interaction between the primary and secondary streams of eject...
A computer program previously developed to analyze three-dimensional supersonic nozzles by the metho...
The ability of analysis to predict ejector nozzle characteristics over a wide range of conditions an...
An analytical procedure for computing the performance of supersonic ejector nozzles is presented. Th...
Flows through three reference nozzles have been calculated to determine the capabilities and limitat...
An experiment was conducted at static conditions to determine the internal performance effects of no...
This paper discusses a test of a nozzle concept for a high-speed commercial aircraft. While a great ...
An investigation was conducted in the model preparation area of the Langley 16-Foot Transonic Tunnel...
Numerous experiments were conducted to determine factors which affect the internal performance of co...
An experimental investigation of a series of four convergent-divergent exhaust nozzles was conducted...
Conventional procedures for designing nozzles involve the design of an inviscid contour (using the m...
Effects of shroud geometry on performance of collapsible plug nozzle at Mach numbers from 0 to 2.
Pumping characteristics of variable geometry ejectors with hot and cold primary nozzle flo
Pumping and internal thrust performance of simulated variable divergent-shroud ejector nozzle design...
An improved ability to predict external propulsive performance was incorporated into the three-dimen...