Cold-flow tests were performed using a simulated Air Augmented Rocket (AAR) operating as a mixer-ejector in order to investigate the effects of varied primary nozzle lip thickness on mixing and entrainment. The simulated primary rocket ejector was supplied with nitrogen at a maximum chamber stagnation pressure of 1712 psi, and maximum flow rate of 1.67 lbm/s. Secondary air was entrained from a plenum, producing pressures as low as 6.8 psi and yielding maximum stagnation pressure ratios as high as 160. The primary ejector nozzles each had an area ratio of approximately 20, yielding average primary exit Mach numbers between 4.34 and 4.57. The primary flow was ejected into an 18.75 inch-long mixing duct with a rectangular cross-sectional area of 2.10 in2. The secondary flow was entrained into the mixing duct through a total cross section of 0.94 in2. Two mixing duct configurations were used, one with plexiglass upper and lower surfaces for flow visualization and one with pressure ports along the lower surface for primary plume measurements. Shadowgraph images were used to characterize the mixing duct flow field, while pressure and temperature instrumentation allowed for calculation of various ejector performance characteristics. Experimentally-calculated performance characteristics were compared to inviscid theoretical predictions. Varying degrees of flow field asymmetry were observed with each nozzle. Test repeatability was found to be excellent for all nozzles. Several distinct phenomena were observed in both the primary plume and secondary streams. The duration of secondary flow choking was found to be inversely proportional to nozzle lip thickness, due to the primary plume being physically closer to the secondary flow with a thinner nozzle lip. This indicated that the ejector’s ability to choke the secondary flow is primarily an inviscid phenomenon. Secondary flow blockage was demonstrated in two consecutive tests using the thickest nozzle lip. Only the left secondary duct became blocked in each case. Blockage was only demonstrated in the centerline pressure configuration, so no visual evidence was able to support the blocked flow theory. At every pressure ratio, entrainment ratio was shown to increase with nozzle lip thickness. The original conical nozzle produced the largest level of entrainment, indicating that the angle of primary flow impingement was the largest contributing factor to secondary entrainment. The increase in efficiency resulting from a bell-mouth nozzle was less than the increase in entrainment efficiency of a conical nozzle, indicating that the conical design was more efficient overall for air augmented rocket applications.

The ejector expansion refrigeration cycle is a modified vapor compression cycle in which a two phase ejector is used to recover a portion of the work otherwise lost in the expansion valve. The ejector improves cycle performance by increasing compressor inlet pressure and by lowering the quality of the fluid entering the evaporator. Theoretically, a cooling COP improvement of approximately 21 % is achievable for a typical refrigerating cycle and an ideal ejector. If the ejector performed as well as typical single-phase ejectors, an improvement of 12% could be achieved. Previous tests have demonstrated a smaller 3.7% improvement; the difference is in the poor performance of the two-phase ejector. The purpose of this research is to understand the operating characteristics of the two phase ejector and to improve design. A two-phase ejector test rig has been constructed and tested. Preliminary data show performance superior to previously tested two-phase ejectors, but still inferior to single phase ejectors. Ejector performance corresponds to refrigeration cycle COP improvements ranging from 3.9010 to 7.6%. This performance was obtained with an ejector designed from single-phase ejector and wet steam ejector design methods. The poor performance indicates the design methods must be improved for two-phase ejectors. This research has begun the development of design methods for the two-phase ejectors and this research has developed models to describe the fluid dynamics and thermodynamics of the ejector. / Ph. D.

No / The results of computational fluid dynamics simulation for convective heat transfer of turbulent flow in a cooled convergent-divergent nozzle are reported. The importance of the heat transfer coefficient is to find the most suitable metals for the nozzle wall as well as its application for producing nano-particles. ansys-icem and ansys-cfx 13.0 are used to mesh and simulate fluid flow in the nozzle, respectively. Effects of grid resolution and different turbulence models on the heat transfer coefficient are investigated. Three turbulence models of k-omega, k-epsilon and shear stress transport are applied to calculate the heat transfer coefficient. Stagnation absolute pressure and temperature are 10.3 bara and 840 K, respectively, the same as those in the experimental work. The heat transfer coefficients obtained from simulation are compared with the available experimental data in literature to find out the best suitable mesh grid and the turbulence model. Under the selected operating conditions, k-epsilon and k-omega models have shown the best agreement with the experimental data with the average error of 6.5% and 10%, respectively, while shear stress transport under predicts the values with 16% error.

<p>Electrostatic spray is a spray that is induced by an interaction between the surface charge on the liquid meniscus and the externally applied electrical field that forms a conical shape known as the Taylor Cone. Electrostatic spray can be seen in a variety of different fields in modern times, such as, agriculture, combustion, space propulsion, and medical applications. The experimental setup for any electrostatic spray consists of the following components: a syringe pump filled with an ionic fluid, a high voltage power supply, and a ground source. The orientation of the nozzle, set to a horizontal or vertical orientation, and the interface that is examined, liquid/air or liquid/liquid interface are two parameters that can vary from one setup to another while still using the same components to form the electrostatic spray. In this experimental study, the characteristic of the electrostatic spray of two immiscible fluids, liquid/liquid interface, with a horizontal nozzle orientation, was analyzed. The two immiscible fluids that were chosen for this experiment were olive oil, the ambient fluid, and pure ethanol, the working fluid. A set range of 0 – 5 kV with an increment of 0.5 kV was applied to the working fluid with a flowrate of 0.1 mL/min. The distance between the nozzle and the copper disk was also altered for three different distances, 22.09, 14.6 and 10.33 mm. Different patterns and trajectories were captured and analyzed using both a high-speed camera and a long exposure camera. Formation of vortices was recorded in the induced flow. The general trend was found was an increase in the droplets’ velocity with the increase of the applied voltage. Additionally, there was an increase in the droplets’ velocity was recorded as the copper disk was moved closer to the nozzle. A dimensional number, Jowaiser’s number Jo, has been proposed where it relates the electric forces to the inertial forces. It can be used to predicts the phase that the flow experiences. The four phases that a flow can experience are the droplet phase, transition phase, spray phase, and the shorting phase.  </p>

This study was regarding the waterjets in the water atomization process. This is because the understanding of the waterjets is not complete and with a greater understanding the production of metal powder could be improved. The waterjets were going to be categorized according to their wave function, size and distribution of the droplets and the three regimes that Höganäs had divided up the jets into was also analyzed. The three regimes depend on the jets characteristics and the regimes are the transparent, milky and the droplet jet. The purpose was to get a better understanding of the correlation between velocity, temperature, waves, size and distribution of the droplets in a 50 cm long waterjet. The method to enhance the understanding of this project was to first do theoretical solution with the help of fluid dynamics. Weber, Reynolds and Ohnesorge number were calculated and evaluated to get a better understanding of the waterjet. Secondly, experiments were conducted where a waterjet with different nozzles and temperatures was filmed with a highspeed camera and the videos were analyzed with the help of a software package called ImageJ. The results show the correlation between increasing temperature and decreasing droplet size and a less cohesive waterjet core. The conclusion from the study was that with the help of temperature one can help control the droplet size. / Denna studie angår vattenstrålar i en vattenatomiserings process vid tillverkning av metallpulver och en bättre förståelse skulle förbättra tillverkningen av metallpulver. Vattenstrålen skulle kartläggas enligt dess vågfunktion, storlek och spridning av dropparna och de tre regionerna som Höganäs har delat upp vattenstrålen i skulle analyseras. Regionerna är beroende av strålens karaktäristiska utseenden vid olika delare av vattenstrålen och är genomskinlig, mjölkig och dropp stråle. Syftet med studien var att få en bättre förståelse av sambandet mellan hastighet, temperatur, vågor, storlek och spridning av dropparna i en 50 cm lång vattenstråle. Metoden som användes för att öka förståelsen av vattenstrålen var först en teoretisk del med hjälp av fluidmekanik. Weber, Reynolds och Ohnesorge tal beräknades och utvärderades för att ge en teoretisk förståelse för vattenstrålen. Sedan utfördes vattenflödesexperiment, där vattenstrålen filmades med olika munstycken och temperaturer med en höghastighetskamera och videon analyserades med hjälp av mjukvaran kallad ImageJ. Resultaten visar ett samband mellan ökad temperatur och minskad droppstorlek och en mer uppbruten kärna av vattenstrålen. Slutsatsen från studien var att man med hjälp av temperaturen kan reglera droppstorleken.

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