Results 71 to 80 of about 18,062 (227)
High‐current interruptions aggravate arc contact ablation, and arcing time strongly influences the gas‐blast capability of self‐energy SF6 circuit breakers. This study quantifies the effect of arcing time on gas flow characteristics while accounting for cumulative arc contact ablation over repeated operations.
Xue Zhang +6 more
wiley +1 more source
The bypass dual-throat nozzle is based on the dual-throat nozzle, which is a fluidic thrust vector nozzle suitable for integration into rocket motors in a symmetrical manner.
Xuefeng Xia +5 more
doaj +1 more source
Chemical species and chemical reactions of importance in nonequilibrium performance calculations [PDF]
Computer programs to determine inviscid one dimensional and axisymmetric nonequilibrium nozzle flow ...
Gold, P. I., Weekley, C. T.
core +1 more source
This study is aimed at addressing combustion instability phenomena observed during the operation of dual‐burn‐rate Solid Rocket Motors (SRM) with a large aspect ratio. Previously, the acoustic mode of the combustion chamber (induced by external excitation) and the vortex shedding frequency were typically analyzed independently, and the probability of ...
Wenhao Yu +6 more
wiley +1 more source
A three-dimensional turbulent compressible flow model for ejector and fluted mixers [PDF]
A three dimensional finite element computer code was developed to analyze ejector and axisymmetric fluted mixer systems whose flow fields are not significantly influenced by streamwise diffusion effects.
Rushmore, W. L., Zelazny, S. W.
core +1 more source
Droplets formation inside a venturi liquid mixer [PDF]
The formation of a coarse photographic emulsion by entraining a hot oil phase into a cooler aqueous phase by a Venturi device is considered. The main focus is on understanding the mechanism and site of droplet formation in the device, as well as the time-
Carnie, S.L., Davidson, M.R.
core
This study presents an in‐depth structural evaluation of the convergent nozzle in a microgas turbine engine (MGTE), focusing on the performance of various lightweight materials used in aerospace applications. The research investigates both structural and aerothermal characteristics of the nozzle under realistic operating conditions.
Darshan Kumar Jayaram +4 more
wiley +1 more source
Interim user's manual for boundary layer integral matrix procedure, version J [PDF]
A computer program for analyzing two dimensional and axisymmetric nozzle performance with a variety of wall boundary conditions is described. The program has been developed for application to rocket nozzle problems.
Evans, R. M., Morse, H. L.
core +1 more source
Entrainment characteristics of unsteady subsonic jets [PDF]
The effectiveness of jet unsteadiness in enhancing flow entrainment was assessed. It was conducted that entrainment depends on the type and amount of jet unsteadiness.
Bremhorst, K. +2 more
core +1 more source
NUMERICAL INVESTIGATION OF CHOCKED CONVERGING-DIVERGING NOZZLES FOR THRUSTER APPLICATION
The need for low-thrust propulsion systems for small scale spacecraft is growing. Low thrust characteristics generally lead to low Reynolds number flows from propulsive devices that utilize converging-diverging nozzle.
Mohd Hafiz Mohd Noh
doaj +1 more source

