… /turbulent-boundary layer interaction inside the nozzle. From purely gas-dynamics point of …
occur and can strongly affect the flow-field inside the nozzle (see Figs. 3, 4). Previous studies …

… nozzle with normal shock at the outlet. In addition to a wave reflected from the nozzle inlet,
the supersonic nozzle … For reasonable values of the nozzle inlet Mach number, the pressure …

… 1) was programmed depending on the type of nozzle, ie 110 flat fan nozzle, 80 flat fan
nozzle or 80 cone nozzle. All measurements were carried out through the long axis of the spray …

… test nozzle used in this investigation was a subscale, nonaxisymmetric, two-dimensional CD
nozzle … Based on one-dimensional theory, the nozzle has a design NPR of 8.78 and an exit …

… rocket nozzle can only be deleterious to the effectiveness of the nozzle expansion process
in converting thermal to kinetic energy. The condensed particles are accelerated in a nozzle …

… Ideally, the overexpanded nozzle flow is supersonic within the entire portion of the nozzle …
However, for an actual nozzle under ambient pressure condition 5, complicated shock wave …

… nozzle exit plane affect conditions within the nozzle. It is found that, when choking of the
compound-compressible flow nozzle … is shown to be choked at the nozzle throat, although the in…

… two-phase nozzle flow compared with those of the one-phase flow are illustrated through
the calculations of the JPL nozzle, the Titan III solid rocket motor, and the submerged nozzle …

… nozzle pressure ratios. The results are compared with available experimental data in a nozzle
… The nozzle area ratioAe=At isfixed at 1.5 and the nozzle divergence angle is 3.89 deg, the …

… effects of spray pressure, airspeed, and nozzle orientation (angle of spray discharge relative
… the velocity of spray exiting a nozzle), in combination with nozzle orientation, was extremely …