• Title/Summary/Keyword: Free Jet

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Centerline Turbulent Characteristics of an Axisymmetric Flow with the Swirl (소용돌이 성분이 있는 축대칭유동의 중심난류 특성)

  • 남경덕;한용운
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.10
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    • pp.2724-2737
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    • 1994
  • The swirl effect on an axisymmetric turbulence has been investigated along its centerline by the hot wire anemometry. Flow facility to generate and conrol the swirl has been built by using the rotating honeycomb and grid. For the case of internal flows, as the strength of the swirl increases the flow tends to be locally isotropic by modifying the radial and the rotational components mainly. In comparison with those of the plain free jet, the decay of the centerline turbulences seems to be delayed substantially even with a slight swirl component.

A study on the change of turbulence structure in a diffuser (확대관의 난류구조 변동에 관한 연구)

  • Lee, Jang-Hwan;Han,Yong-Un
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.21 no.4
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    • pp.503-508
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    • 1997
  • The change of the structure of homogeneous turbulence subject to irrotational strains has been studied in an anti-Morel type diffuser (center matched cubic contour) using the hot wire anemometry. It was observed that the profiles of mean velocities and turbulence velocities along the center line were stable at the entrance region but rapidly changed near the matching point. The wall induced turbulence at the entrance region grows fast and was diffused toward the center at downstream. It was also observed that the axial turbulence grows faster than the radial one in the middle region of the diffusing flow and that the diffusing process has the vortex compression mechanism due to the conservation of angular momentum. These phenomena are frequently observed at the initial flow region of the free jet.

Combustion Characteristics of Hypersonic SCRamjet Engine (극초음속 스크램제트 엔진의 연소특성)

  • Won, Su-Hee;Jeong, Eun-Ju;Jeung, In-Seuck;Choi, Jeong-Yeol
    • 한국연소학회:학술대회논문집
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    • 2003.12a
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    • pp.159-165
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    • 2003
  • This paper describes numerical efforts to characterize the flame-holding and air-fuel mixing process of model SCRamjet engine combustor, where a hydrogen jet injected into a supersonic cross flow and in a cavity. Combustion phenomena in a model SCRamjet engine, which has been experimentally studied at University of Queensland and Australian National University using a free-piston shock tunnel, was observed around separation region of upstream of the normal injector and inside of cavity. The results show that the separation region and cavity generates several recirculation zones, which increase the fuel-air mixing. Self ignition occurs in the separation-freestream and cavity-freestream interface.

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An Experimental Study on Slamming Phenomenon by Forced Impact (강제 입수에 의한 슬래밍 현상에 관한 실험적 연구)

  • Nahm, Jong-Ou;Kang, Hyo-Dong;Chung, Jang-Young;Kwon, Sun-Hong;Choi, Han-Suk
    • Journal of Ocean Engineering and Technology
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    • v.21 no.1 s.74
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    • pp.40-44
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    • 2007
  • This paper presents the experimental results on slamming phenomenon. The air pressure cylinder was used to ensure repeatability of the impact. The results showed that the adopted experimental technique was excellent in terms of repeatability, compared to that of the free drop tests. The pressure time histories, magnitude of peak pressure and the behavior of jetspray were obtained. The flat specimen was tested for various incident angles. To estimate the incident speed of the specimen, a high-speed camera was used. The high-speed camera was also a useful tool in understanding the behavior.

Alternative practices of achieving anaesthesia for dental procedures: a review

  • Angelo, Zavattini;Polyvios, Charalambous
    • Journal of Dental Anesthesia and Pain Medicine
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    • v.18 no.2
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    • pp.79-88
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    • 2018
  • Managing pain and anxiety in patients has always been an essential part of dentistry. To prevent pain, dentists administer local anaesthesia (LA) via a needle injection. Unfortunately, anxiety and fear that arise prior to and/or during injection remains a barrier for many children and adults from receiving dental treatment. There is a constant search for techniques to alleviate the invasive and painful nature of the needle injection. In recent years, researchers have developed alternative methods which enable dental anaesthesia to be less invasive and more patient-friendly. The aim of this review is to highlight the procedures and devices available which may replace the conventional needle-administered local anaesthesia. The most known alternative methods in providing anaesthesia in dentistry are: topical anaesthesia, electronic dental anaesthesia, jet-injectors, iontophoresis, and computerized control local anaesthesia delivery systems. Even though these procedures are well accepted by patients to date, it is the authors' opinion that the effectiveness practicality of such techniques in general dentistry is not without limitations.

Supersonic Free Jet and Ab initio Studies of Electronic-Vibrational Structures of Fluorene

  • 부봉현;최영식;김택수;강성권;김재룡
    • Bulletin of the Korean Chemical Society
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    • v.16 no.4
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    • pp.341-344
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    • 1995
  • Laser-induced fluorescence (LIF) excitation spectra were measured for fluorene (FR) cooled in pulsed supersonic expansions of He in the range 283.7-296.7 nm. Ab initio studies of FR have also been carried out for determining the electronic and vibrational structures by using the standard 3-21G basis sets. In the LIF excitation spectra of FR, highly resolved vibronic bands are observed having the band origin of 33,791 cm-1. The vibrational bands above the electronic origin were assigned on the basis of the well-characterized electronic vibrational bands reported previously and of normal modes of vibrations derived by our HF/3-21G calculations.

A Experimental Study on the Effect of Increasing Rudder Force on Turning Ability of Short Sea Shipping Ship (타력 향상이 근해운송선박의 선회 성능에 미치는 영향에 관한 실험적 연구)

  • Jun, Hee-Chul;Kim, Sang-Hyun;Kim, Hyun-Jun;Park, Hwa-Pyeong
    • Journal of the Korean Society of Marine Environment & Safety
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    • v.18 no.6
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    • pp.591-596
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    • 2012
  • Recently, a vessel's maneuvering performance is considered to be an important subject to secure safety at short sea shipping. Especially the high turning performance, which is required to avoid the marine pollution by the ships that was grounded, becomes more severe. In this paper, we discuss the effect of increasing rudder force on turning performance of short sea shipping ship by free running test in towing tank. First of all, we make the 47K PC model ship and high-lift rudder using Coanda effect. And we make the free running test system for the turning test in towing tank. And also we perform the turing test of 47K PC model in several changes of Coanda jet momentum and evaluate the turing performance such as advance and tactical diameter. Finally, we confirm that the increasing of rudder force is very effective to improvement of turning performance of short sea shipping ship.

Surface Modification with Atmospheric Microwave Agron Plasma Jet Assisted with Admixture of H2O2 and Analysis of Plasma Characteristics

  • Won, I.H.;Shin, H.K.;Kwon, H.C.;Kim, H.Y.;Kang, S.K.;Lee, J.K.
    • Proceedings of the Korean Vacuum Society Conference
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    • 2013.02a
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    • pp.544-545
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    • 2013
  • Recently, low-temperature atmospheric-pressure plasmas have been investigated [1,2] for biomedical applications and surface treatments. Experiments for improving hydrophilicity of stainless steel (SUS 304) plate with atmospheric microwave argon and H2O2 mixture plasma jet [3] were carried out and experimental measurements and plasma simulations were conducted for investigating the characteristics of plasma for the process. After 30 s of low power (under 10 W) and low temperature (under $50^{\circ}C$) plasma treatment, the water contact angle decreased rapidly to around $10^{\circ}$ from $75^{\circ}$ and was maintained under $30^{\circ}$ for a day (24 hours). The surface free energy, calculated from the contact angles, increased. The chemical properties of the surface were examined by X-ray Photoelectron Spectroscopy (XPS) and the surface morphology and roughness were examined by Scanning Electron Microscopy (SEM) and Atomic Force Microscopy (AFM) respectively. The characteristics of plasma sources with several frequencies were investigated by Optical Emission Spectroscopy (OES) measurement and one-dimensional Particle-in-Cell (PIC) simulation and zero-dimensional global simulation [4]. The relation between plasma components and the efficacy of the surface modification were discussed.

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Thermomechanical Effect on the Water Wet Dental Hard Tissue by the Q-switched Er : YAG Laser

  • Y. H. Kwon;Ky0-han Kim
    • Journal of Biomedical Engineering Research
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    • v.20 no.2
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    • pp.231-236
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    • 1999
  • Understanding the exgenous water induced thermomechanical effect on the dental hard tissue by the Q-switched Er:YAG laser (1-$mutextrm{s}$-long pulse width) has an important impact on the further understanding of the free-running Er:YAG laser (250-$mutextrm{s}$-long pulse width) ablation on the dental gard tissue because one macroscopic effect in the free-running laser is an accumulation of microscopic effects we investigated in this study. The Q-switched Er:YAG laser with exogenous water on the tooth enhanced ablation rate compared to the case of no water on the tooth. The frequency of exogenous-water jet on the tooth has affected the ablation rate in such a way that as we dispensed water drops less frequently we could get more enhanced ablation rate. The amplitude of the recoil pressure depends on the tooth surface conditions such that as surfaces wet, and as the volume of the exogenous water drop increased, the amplitude of the recoil pressure increased also. From this study we realized that the 1 $mutextrm{s}$ long pulsed induced thermomechanical effect provides us useful information for the understanding of the free-running Er:YAG laser induced ablation with exogenous water.

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Experimental Investigation for the Shroud Separation in the Supersonic Flow (초음속 비행환경 조건에서의 슈라우드 분리시험 연구)

  • Kim, Jung-Young;Lee, Dong-Min
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.45 no.7
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    • pp.539-549
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    • 2017
  • In this paper, experimental studies on the shroud separation were performed to investigate characteristics of the shroud separation at mach 3. Shroud separation tests were carried out in the vertical free-jet wind tunnel that is capable of testing separable structures. A shroud model was miniaturized to meet test objectives and test section dimensions of the wind tunnel. Pneumatic Locking and separation mechanisms were designed considering external force due to free stream. High speed cameras were used to record the shroud motion and unsteady shock patterns over the deploying shrouds during the shroud separation process. Also, unsteady pressures on the nose surface were measured by using the pressure sensors. Through the tests, the measurement data necessary for researches on the shroud separation technology were obtained. Shroud separation behaviors and characteristics of unsteady pressure on the nose surface for each external flow conditions were analyzed.