A time-iterative full Navier-Stokes code, PARC, is used to analyze the flowfield of a two-dimensional ejector nozzle system. A parametric study was performed for two controlling parameters, duct to nozzle area ratio and nozzle pressure ratio. Results show that there is an optimum area ratio for the efficient pumping of secondary flow. At high area ratios, a freestream flow passes directly through the mixing duct without giving adequate pumping. At low area ratios, the jet boundary blocks the incoming flow. The nozzle pressure ratio variation shows that the pumping rate increases as the pressure ratio increases, provided there is no interaction between the shroud wall and the shock cell structure
The Wind computational fluid dynamics code was used to perform a series of simulations on two offset...
Supersonic nozzles which operate at low Reynolds numbers and have large expansion ratios have very t...
Supersonic cruise exhaust nozzles for advanced applications are optimized for a high nozzle pressure...
A three-dimensional full Navier-Stokes (FNS) analysis was performed on a mixer/ejector nozzle design...
Flows through three reference nozzles have been calculated to determine the capabilities and limitat...
An analytical procedure for computing the performance of supersonic ejector nozzles is presented. Th...
A theoretical analysis of the viscous interaction between the primary and secondary streams of eject...
The factors which influence the design and selection of a nozzle for a hypersonic scramjet are descr...
The PARC2D code has been selected to analyze the flowfields of a representative hypersonic scramjet ...
The nozzle is a mechanical device that uses pressure energy and fluid enthalpy to increase the outfl...
A comparison of the NPARC, PAB, and WIND (previously known as NASTD) Navier-Stokes solvers is made f...
International audienceSupersonic ejectors are flow devices of rugged and simple construction, used t...
A general program was conducted to develop and assess a computational method for predicting the flow...
The transonic performance of a dual-throat, single-expansion-ramp nozzle (SERN) was investigated wit...
A second order numerical method employing reference plane characteristics has been developed for the...
The Wind computational fluid dynamics code was used to perform a series of simulations on two offset...
Supersonic nozzles which operate at low Reynolds numbers and have large expansion ratios have very t...
Supersonic cruise exhaust nozzles for advanced applications are optimized for a high nozzle pressure...
A three-dimensional full Navier-Stokes (FNS) analysis was performed on a mixer/ejector nozzle design...
Flows through three reference nozzles have been calculated to determine the capabilities and limitat...
An analytical procedure for computing the performance of supersonic ejector nozzles is presented. Th...
A theoretical analysis of the viscous interaction between the primary and secondary streams of eject...
The factors which influence the design and selection of a nozzle for a hypersonic scramjet are descr...
The PARC2D code has been selected to analyze the flowfields of a representative hypersonic scramjet ...
The nozzle is a mechanical device that uses pressure energy and fluid enthalpy to increase the outfl...
A comparison of the NPARC, PAB, and WIND (previously known as NASTD) Navier-Stokes solvers is made f...
International audienceSupersonic ejectors are flow devices of rugged and simple construction, used t...
A general program was conducted to develop and assess a computational method for predicting the flow...
The transonic performance of a dual-throat, single-expansion-ramp nozzle (SERN) was investigated wit...
A second order numerical method employing reference plane characteristics has been developed for the...
The Wind computational fluid dynamics code was used to perform a series of simulations on two offset...
Supersonic nozzles which operate at low Reynolds numbers and have large expansion ratios have very t...
Supersonic cruise exhaust nozzles for advanced applications are optimized for a high nozzle pressure...