• Journal of Energy Engineering
• /
• v.10 no.3
• /
• pp.272-277
• /
• 2001

An experimental study of jet impinging the non-isothermal heating surface with linear temperature gradient is conducted with the presentation of the turbulent flow characteristics and the heat transfer rate, represented by the Nusselt number. The jet Reynolds number ranges from 15,000 to 30,000, the temperature gradient of the plate is 2~4.2$^{\circ}C$/cm and the dimensionless nozzle to plate distance (H/D) is from 2 to 10. The results show that the peak of heat transfer rate occurs at the stagnation point, and the heat transfer rate decreases as the radial distance from the stagnation point increases. A remarkable feature of the heat transfer rate is the existence of the second peak. This is due to the turbulent development of the wall jet. Maximum heat transfer rate occurs when the axial distance from the nozzle to nozzle diameter (H/D) is 6 or 8. The heat transfer rate can be correlated as a power function of Prandtl number, Reynolds number, the dimensionless nozzle to plate distance (H/D) and temperature gradient (dT/dr). It has been found that the heat transfer rate increases with increasing turbulent intensity. The wall jet is influenced by temperature gradient and the effect becomes more important at higher radii.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.34 no.6
• /
• pp.51-58
• /
• 2006

The spray characteristics of liquid jet injected into subsonic cross-flow were investigated experimentally. Spray trajectories were captured using CCD camera. Droplet sizes were measured using PDPA and Image Express. The nozzle diameter was 0.5 mm, and its length-to-diameter ratios (L/D) ran$4.11{\times}10^6$ged from 1.0 to 6.0. Experimental results indicate that the breakup point is delayed by increasing gas momentum ratio and the penetration length is decreased by increasing Weber number. At low injection angle(${\theta}$ < $90^{\circ}$), Weber number is dominant parameter for trajectories, but at high injection angle(${\theta}$ > $90^{\circ}$), L/D is dominant parameter for trajectories rather than Weber number.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.7 no.2
• /
• pp.7-14
• /
• 2003

Computational work using the axisymmetric, compressible, Navier-Stokes Equations is carried out to predict the discharge coefficient of mass flow through a micro-critical nozzle. Several kinds of turbulence models and wall functions are employed to validate the computational predictions. The computed results are compared with the previous experimented ones. The present computations predict the experimental discharge coefficients with a reasonable accuracy. It is found that the standard $\kappa$-$\varepsilon$turbulence model with the standard wall function gives a best prediction of the discharge coefficients. The displacement thickness of the nozzle wall boundary layer is evaluated at the nozzle throat and is well compared to a prediction obtained by an empirical equation. The resulting displacement thickness of the wall boundary layer is about 2% to 0.6% of the diameter of the nozzle throat for the Reynolds numbers of 2000 to 20000.

• Journal of the Korean Institute of Gas
• /
• v.25 no.6
• /
• pp.22-28
• /
• 2021

Combustion characteristics were examined experimentally for a swirl-stabilized double cone premixed burner nozzle used for industrial gas turbines for power generation. An original model and a variant with a different fuel injection pattern are tested to compare their combustion characteristics such as NOx, CO and stability in pressurized conditions with single burner-flame and in an ambient multi-flame conditions with multi-burners. Test results show that NOx emissions are smaller for the variant, whose number of fuel holes is reduced with the same total area of fuel holes, in ambient and pressurized single-flame conditions with single burner, which results from enhanced fuel/air mixing due to a higher penetration of fuel into the air stream. The multi-burnerflame test results show that NOx emissions are smaller for the variant due to reduced flame interactions, which, on the contrary, slightly reduces the stability margin. On-site test results fromin an actual power plants also show that NOx emissions are reduced for the variant, compared with the original one, which is in agreement with the lab test results stated above.

• Journal of Biosystems Engineering
• /
• v.21 no.2
• /
• pp.146-154
• /
• 1996

농약의 직주입 혼합방식은 작업자의 안전에 기여하며 남은 농약은 용기와 함께 수거되어 재사용 되므로 환경보전 및 경제적 이점이 있다. 그러나 주입식 방제기의 분관내 농약혼합액이 노즐에 이르는 시간까지의 유동특성인 지연시간은 농약 살포량에 오차를 유발한다. 본 연구는 이 지연시간이 미치는 실제 살포오차의 정도를 파악하려 시뮬레이션을 행하였다. 시뮬레이션의 결과에 의하면 오차는 상당히 심각한 것으로 판단되었으며 지연시간을 단축하려는 여러 방법을 검토하였다. 분관의 직경을 줄여 유동속도를 빠르게 하거나, 혼입 농약의 양을 일정하게 유지하며 방제속도를 가능한 목표속도에 맞추는 방법 등은 약간의 오차를 줄일 수 있을 뿐이었고, 농약을 각 노즐에 주입함으로써 오차를 최소화할 수 있으나 미소계략의 문제를 내포하였다. 따라서 농도의 변화에 따른 지연시간을 없앤 직주입 총유량 제어방식을 통하여 노즐 배출유량을 방제속도의 변이에 따라 보상하며 비례적으로 농약을 주입하여 농도를 일정하게 유지할 수 있을 것으로 판단된다.

• Proceedings of the Korean Vacuum Society Conference
• /
• 2011.02a
• /
• pp.481-481
• /
• 2011

이 논문은 세라믹 노즐(내경: 20 um)을 제작하여 새로운 프린팅 방식인 정전기수력학방식을 이용하여 유리기판위에 직경 30 um의 ZnO seed dot를 패턴하였다. 정전기수력학은 기존의 프린팅 방식과 달리 전기장으로 유도된 노즐을 이용하여 액적을 토출시키는 새로운 프린팅 방법이다. 패턴된 ZnO seed는 열처리후 수열합성법을 이용하여 성장시켰다. 같은 방법으로 잉크젯 프린팅을 이용하여 ZnO seed 패턴 후 열처리하여 수열합성을 이용하여 성장시켰다. 잉크젯 프린팅 방식을 이용하여 성장된 ZnO nanowire는 위성 액적이 떨어져 ZnO seed dot 주변에 ZnO nanowire가 성장하였다. 반면, 정전기수력학 프린팅 방식을 이용하여 성장된 ZnO nanowires는 ZnO seed 패턴 중앙에 집중되어 ZnO nanowire가 성장하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.35 no.8
• /
• pp.706-713
• /
• 2007

The jet structure issuing from a conventional convergent nozzle of variable expansion rate is compared with the result from the nozzle of a constant expansion rate using a normal type annular slit. In experiments, to investigate the jet characteristics between the two cases of jet, the mean velocity of nozzle exit is fixed to be 90m/s, the pressures along the jet axis and radial directions are measured by a scanning valve system moving with 3-axis auto-traverse unit, and the velocity distribution obtained by calculation from the measured static and total pressures is compared. Also to obtain the highly stable and convergence jets, it is turned out that the flow through a nozzle of constant expansion rate using the Coanda effect with an annular slit is the most preferable than that case through variable expansion rate nozzle. Furthermore, it is found that the pressure drop along the nozzle for the constant expansion rate nozzle is small relatively against to the case of variable expansion rate nozzle.

• Journal of Energy Engineering
• /
• v.22 no.4
• /
• pp.413-419
• /
• 2013

The present study used the MILD combustor, which has coaxial cylindrical tube. The outside tube of the MILD combustor corresponds to the exhaust gas passage and the inner side tube is the furnace passage. A numerical analysis was accomplished to elucidate the characteristics of exhaust gas entrainment toward the inner furnace with the changes of venturi nozzle geometrical parameters, nozzle position, nozzle gap between high pressure air nozzle and venturi nozzle, and with the change of high pressure nozzle inlet velocity. The entrainment flow rate for the case with the high pressure air nozzle attached at the exhaust gas wall has relatively small change with the change of nozzle gap. That for the case with the high pressure air nozzle exposed to the exhaust gas has monotonically increase with the change of nozzle gap. The flow rate ratio of entrainment flow rate has considerably increase tendency with relatively lower air inlet velocity, on the other hand, that with relatively higher air inlet velocity could be seen relatively small increase.

• Journal of Energy Engineering
• /
• v.18 no.4
• /
• pp.258-263
• /
• 2009

Jet Loop Reactor(JLR), in which a two-phase nozzle is installed, is the new design technique for the treatment of high concentration wastewater by accelerating of oxygen contacting between substrate and surrounding bacteria. This numerical study of the two phase jet flow was conducted to find the optimum design of JLR. It was shown that there was a minimum velocity in the nozzle for continuous circulation of wastewater. The optimum location and the size of the draft tube for continuous circulation were examined. It was certain that the smaller the air size is, the more the effect of the mixing increases. The relation between the mixing effect and the turbulence was confirmed.

• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2009.05a
• /
• pp.149-152
• /
• 2009

Spray characteristic parameters such as droplet mean velocity, diameter, and volume flux are measured at various locations of spray in order to investigate the evolutionary feature of droplets exiting from a direct-injection type thruster nozzle-orifice. The experimental results indicate that the large droplets with high velocity at the center of upstream are broken-up into smaller droplets with low velocity due to their continuous momentum loss to surrounding air along with spray evolution toward downstream. Also it is found that the high volume flux expands its distribution in radial direction as a results of spray spreading and dispersion.