• Title/Summary/Keyword: 선회 시험

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Permanent Deformation Properties of Porous Pavement Modified by Pyrolysis Carbon Black (열분해 카본블랙을 이용한 배수성 아스팔트 혼합물의 소성변형 특성)

  • Lee, Kwan-Ho
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.15 no.6
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    • pp.3888-3893
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    • 2014
  • The number of waste tires is increasing. One effective recycling method is the pyrolysis of waste tires. Using the pyrolyzed carbon black from waste tires, the characteristics of permanent deformation for PA-13mm porous mixture were evaluated. The confining pressure of 138 kPa and deviatoric stress of 551 kPa were adopted. The testing temperature was $45^{\circ}$ and 50 gyrations of the gyratory compactor was used to simulate the medium traffic level. The mixture modified by 10% PCB showed the largest Marshall Stability of 3.41 kN. The stability of the mixtures with PCB was 50% higher than that of mixture without PCB. The limited laboratory test showed that the use of PCB in a porous pavement decreases the permanent deformation and will be an effective alternative method to reducing the permanent deformation of a porous pavement.

A Study on Application of Warm-Mix Quiet Pavement Using Fine-Size Aggregate (소입경 골재를 이용한 중온 저소음 아스팔트 포장의 적용 연구)

  • Jo, Shinhaeng;Baek, Yujin;Kim, Nakseok
    • Journal of the Society of Disaster Information
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    • v.9 no.1
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    • pp.56-64
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    • 2013
  • The study examines the quiet pavement using fine-size aggregates and warm-mix technique to reduce traffic noise. In order to evaluate the quality of pavement, mix design and laboratory tests were carried out. Test results showed that using 10mm aggregates can reduce the cantabro loss compared with 13mm aggregates due to increase contact area between aggregates. Mixing and compaction temperatures of warm mix quiet pavement should be determined by gyratory compactor test because it is used high viscosity asphalt binder. Using warm-mix additive could reduce compaction temperature by about $15^{\circ}C$. Noise measurement and permeability tests were conducted at the test road for evaluation of the field performance. All of quiet pavements meet the standard of permeability and have sufficient porosity. Noise reduction of the quiet pavement using fine-size aggregates is more effective than that using 13mm aggregates. In particular, the effect of noise reduction was noticeable at low speeds.

Combustion Characteristic Study of LNG Flame in an Oxygen Enriched Environment (산소부화 조건에 따른 LNG 연소특성 연구)

  • Kim, Hey-Suk;Shin, Mi-Soo;Jang, Dong-Soon;Lee, Dae-Geun
    • Journal of Korean Society of Environmental Engineers
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    • v.29 no.1
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    • pp.23-30
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    • 2007
  • The ultimate objective of this study is to develop oxygen-enriched combustion techniques applicable to the system of practical industrial boiler. To this end the combustion characteristics of lab-scale LNG combustor were investigated as a first step using the method of numerical simulation by analyzing the flame characteristics and pollutant emission behaviour as a function of oxygen enrichment level. Several useful conclusions could be drawn based on this study. First of all, the increase of oxygen enrichment level instead of air caused long and thin flame called laminar flame feature. This was in good agreement with experimental results appeared in open literature and explained by the effect of the decrease of turbulent mixing due to the decrease of absolute amount of oxidizer flow rate by the absence of the nitrogen species. Further, as expected, oxygen enrichment increased the flame temperatures to a significant level together with concentrations of $CO_2$ and $H_2O$ species because of the elimination of the heat sink and dilution effects by the presence of $N_2$ inert gas. However, the increased flame temperature with $O_2$ enriched air showed the high possibility of the generation of thermal $NO_x$ if nitrogen species were present. In order to remedy the problem caused by the oxygen-enriched combustion, the appropriate amount of recirculation $CO_2$ gas was desirable to enhance the turbulent mixing and thereby flame stability and further optimum determination of operational conditions were necessary. For example, the adjustment of burner with swirl angle of $30\sim45^{\circ}$ increased the combustion efficiency of LNG fuel and simultaneously dropped the $NO_x$ formation.

Hydrothermal crystallization and secondary synthesis of vanadium containing zeolites (바나듐함유 제올라이트의 수열결정화 및 2차처리합성)

  • Kim, Geon-Joong
    • Journal of the Korean Crystal Growth and Crystal Technology
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    • v.7 no.3
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    • pp.437-448
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    • 1997
  • The substitution of vanadium atoms into the zeolite framework structure could be applied to the large pore zeolites by means of modified treatments as well as direct hydrothermal synthesis. The incorporation of V into the zeolite framework was demonstrated by instrumental analysis techniques. The result of X-ray diffraction analysis showed that the unit cell parameters increased after incorporation of vanadium into the zeolitic lattice, indicating that the replacement of Si by the larger V atoms could cause a slight expansion in the unit cell. In addition, the results of FTIR, Uv-Vis and Si-MAS-NMR spectra strongly support the incorporation of V into the zeolite framework. Acid leaching of aluminum in zeolites can provide a vacant position in the lattice for the insertion of vansdium by secondary hydrothermal treatment.

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A Study on the Method of Turning Circle Drawing by Z-test (Z시험에 의한 선회권의 작도법에 관한 연구)

  • 오정철
    • Journal of the Korean Institute of Navigation
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    • v.7 no.1
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    • pp.33-62
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    • 1983
  • A navigator on bridge needs to know every kinds of motion characteristics of his vessel at sea. Generally when a vessel is completely built, the shipyard makes turning circle diagrams from the results of turing circle tests made during the sea trials for the reference of the vessel's owner. But referring only the data of a turning circle diagram, an officer on bridge can not figure out his vessel's maneuvering characteristics sufficiently, So nowadays the shipyard often adds Z test to turning circle test for more detail references. In this paper the author made Z and turning circle tests at the rudder angles of 15 and and 35 degress separately and in each of the case made a turrning circle diagram from the results of the turning circle test and the esults numerically calculated from mathematical formula made on the base of the maneuvering indices got from the Z test and compared them each other for the purpose of finding the correlations between them. Followings are concluded from the results. An actual turning circle diagram and a calculated one from the results of the Z test at same rudder angle coincides each other well when the center of the calculated circle is transferred by 1.7B toward the direction of the initial turning perpendicularly to the original course and 0.5L toward the direction in parallel with original course in case of the rudder angle of 35 degrees and 1.2B and 0.3L toward each of the above mentioned directions in case of rudder angle of 15 degrees.

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Study on Vehicle Stability Enhancement for the PACE Formula Vehicle (PACE 경주용 차량의 조종안정성 개선에 대한 연구)

  • Kim, Kwan-Ju;Kim, Hyun-Jun;Lee, Jun-Heon
    • Transactions of the Korean Society of Automotive Engineers
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    • v.19 no.1
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    • pp.25-31
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    • 2011
  • The purpose of the study is to enhance the vehicle handling stability of the PACE formula vehicle. Required data for the dynamic analysis of the vehicle are as follows: Mass, moment of inertia, and tire's dynamic properties. Mass and moment of inertia data were calculated using Siemens NX 5.0 which results were verified with VIMF measurements of GMDAT. Dynamic data for the tire were supplied by Kumho Tire. Aerodynamic forces play an important role in the formula vehicle which forces were calculated by using Fluent. Full vehicle dynamic analysis using Carsim software has been carried out to find out the improvement of the vehicle stability by changing the shapes of the rear wing.

Performance Test of A Reverse-Annular Type Combustor (TS2) for APU (보조동력장치용 환형 역류형 연소기 (TS2) 성능 시험)

  • Ko, Young-Sung;Han, Yeoung-Min;Yang, Soo-Seok;Lee, Dae-Sung;Yun, Sang-Sig;Choi, Sung-Man
    • Proceedings of the KSME Conference
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    • 2001.06d
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    • pp.840-845
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    • 2001
  • Development of a small gas-turbine combustor for 100kW class APU(Auxiliary Power Unit) has been performed. This combustor is a reverse-annular type and has a tangential swirler in the liner head to improve the fuel/air mixing and flame stability. Three main and three pilot fuel injectors of the simplex pressure-swirl type are used. The performance target at the design condition includes a turbine inlet temperature of 1170K, a combustion efficiency of 99%, a pattern factor of 30%, and an engine durability of 3000 hours. Under developing the combustor, we conducted performance test of our first prototype(TS1) with some variants. As a result of the test, the performance targets of the combustor are satisfied except that the pattern factor is about 4% higher than target value. So, we redesigned the second prototype(TS2) and conduct performance test with the critical focus on pattern factor and exit mean temperature. We adopted TS2 four variant to check the improvement of pattern factor. As the result, the pattern factors of several variants were satisfied with the performance target. Finally, We chose the TS2A variant as a final combustor for our APU model.

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Circular Motion Test Simulation of KVLCC1 Using CFD (CFD를 이용한 KVLCC1의 Circular Motion Test 시뮬레이션)

  • Shin, Hyun-Kyoung;Jung, Jae-Hwan
    • Journal of the Society of Naval Architects of Korea
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    • v.47 no.3
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    • pp.377-387
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    • 2010
  • In this study, the turbulent free surface around KVLCC1 employed in the circular motion test simulation is numerically calculated using a commercial CFD(Computational Fluid Dynamics) code, FLUENT. Also, hydrodynamic forces and yaw moments around a ship model are calculated during the steady turning. Numerical simulations of the turbulent flows with free surface around KVLCC1 have been carried out by use of RANS equation based on calculation of hydrodynamic forces and yaw moments exerted upon the ship hull. Wave elevation is simulated by using the VOF method. VOF method is known as one of the most effective numerical techniques handling two-fluid domains of different density simultaneously. Boundary layer thickness and wake field are changed various yaw velocities of ship model during the steady turning. The calculated hydrodynamic forces are compared with those obtained by model tests.

The Effect of STPP on Compressive Strength of Sodium Silicate-Cement Grout (STPP가 규산계 시멘트 주입재의 강도에 미치는 영향)

  • Chun, Byungsik;Yang, Hyungchil
    • Journal of the Korean GEO-environmental Society
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    • v.7 no.4
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    • pp.25-34
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    • 2006
  • Portland cement and sodium silicate are widely used as the main components of the injection, which are used to prevent flow and improve ground condition. The main problem of the injection material is the leaching of the sodium hydroxite and silicate due to the limited reaction with the cement. This paper studies the effect of cement hydration retarder on the compressive strength of the sodium silicate - cement gel. A series of tests, including digital-type testing machine, X-ray diffraction and scanning electron microscope are performed. Results clearly demonstrate that the sodium tripolyphosphate, which is the cement hydration retarder in the test, significantly improves the initial strength of the homogel.

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Film Cooling Modeling for Combustion and Heat Transfer within a Regeneratively Cooled Rocket Combustor (막냉각 모델을 이용한 재생냉각 연소기 성능/냉각 해석)

  • Kim, Seong-Ku;Joh, Mi-Ok;Choi, Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.636-640
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    • 2011
  • Film cooling technique has been applied to effectively reduce thermal load on liquid rocket combustion chambers by direct injection of a portion of propellant, which flows through the regeneratively cooling channels, into the chamber wall. This study developed a comprehensive model to quantitatively predict the effects of kerosene film cooling on propulsive performance and wall cooling at supercritical pressure conditions, and assessed the predictive capability against hot-firing tests of an actual combustor. The present model is expected to be utilized as a design and analysis tool to meet the conflicting requirements in terms of performance, cooling, pressure loss and weight.

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