• Title/Summary/Keyword: 고속모형시험

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Reliability-Based Safety and Capacity Evaluation of High-Speed Railroad Bridges (신뢰성에 기초한 고속철도 교량의 안전도 및 내하력평가)

  • 조효남;곽계환
    • Computational Structural Engineering
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    • v.10 no.3
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    • pp.133-143
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    • 1997
  • In Korea, the construction of the first high-speed railroad on the Seoul-Pusan Corridor has already started 3 years ago, in the paper, an attempt is made to develop reliability-based safety and capacity evaluation models for the computer-aided maintenance of the high-speed railroad bridges. The strength limit state models of PC railroad bridges for reliability analysis encompass both the single failure mode such as bending or shear strength and the combined interaction equations which simultaneously take into account flexures, shear and torsion. Then, the actual load carrying capacity and the realistic safety of bridges are evaluated using the system reliability-based equivalent strength, and the results are compared with those of the element reliability based or conventional methods. It is concluded that the proposed models may be appropriately applied in practice for the realistic assessment of safety and capacity of high-speed railroad bridges.

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An Experimental Study on Roll-Damping Characteristics of a Finned Spinning Projectile (회전발사체 미익형상 롤댐핑 특성에 관한 실험연구)

  • Oh, Se-Yoon;Lee, Do-Kwan;Kim, Sung-Cheol;Kim, Sang-Ho;Ahn, Seung-Ki
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.10
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    • pp.894-900
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    • 2012
  • The purpose of this research is to investigate the dynamic roll-damping characteristics of a spin-stabilized projectile in wind-tunnel testing. In the present work, the high-speed wind-tunnel tests for the roll-damping measurements were conducted on a finned spin-stabilized projectile model in the Agency for Defense Development's Trisonic Wind Tunnel at spin rates about 8,000 rpm. The test Mach numbers ranged from 0.6 to 0.9, and the angles of attack ranged from 0 to +15 deg. The evaluation of the bearing friction parameter was also conducted to eliminate the tare damping moment from the aerodynamic damping moment.

Calculation of Wave Resistance of a Hybrid Hydrofoil (복합지지형 고속선의 조파저항 계산)

  • Yoo, J.H.;Kim, Y.G.;Lew, J.M.
    • Journal of the Society of Naval Architects of Korea
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    • v.33 no.1
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    • pp.1-8
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    • 1996
  • A potential-based panel method has been developed for numerical computation of wave resistance on a hybrid hydrofoil. Hybrid hydrofoil is composed of a main body, two struts and two hydrofoils. The main body, which is assumed to be an axisymmetric body for the present analysis, is normally used to support displacement of a body with its buoyancy. Normal dipoles and the sources are distributed on the body(main body, struts, hydrofoils) and the sources are distributed on the free surface. Linearized free surface and the radiation conditions are satisfied using the fourth order finite difference operator and the semi-linear pressure Kutta condition is used for the numerical computation of the hydrofoils. Poisson type free surface condition has been used for the numerical computation and hyperboloidal panel method has been used for better numerical accuracy. To verify this numeric method, model tests are performed in circulation water channel. From the comparison of experimental results with numeric ones, the present method can be used as a useful tool for the design of high speed vessels.

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Measurement and Analysis for the Upper Side Flow Boundary Layer of a High Speed Train Using Wind Tunnel Experiments with a Scaled Model (축소모형 풍동시험을 이용한 고속열차의 유동 상부경계층 측정 및 분석)

  • Oh, Hyuck Keun;Kwon, Hyeok-bin;Kwak, Minho;Kim, Seogwon;Park, Choonsoo
    • Journal of the Korean Society for Railway
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    • v.19 no.1
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    • pp.11-19
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    • 2016
  • The flows around a high speed train are very important because they could affect the aerodynamic characteristics such as drag and acoustic noise. Especially the boundary layer of flows could represent the characteristic of flows around the high speed train. Most previous studies have focused on the boundary layer region along the train length direction for the side of the train and underbody. The measurement and analysis of the boundary layer for the roof side is also very important because it could determine the flow inlet condition for the pantograph. In this study, the roof boundary layer was measured with a 1/20 scaled model of the next generation high speed train, and the results were compared with full-scaled computational fluid dynamics results to confirm their validity. As a result, it was confirmed that the flow inlet condition for the pantograph is about 85% of the train speed. Additionally, the characteristics of the boundary layer, which increases along the train direction, was also analyzed.

Study of Hull Form Development of Wave-Piercing-Type High-Speed Planing Boat (파랑관통형 고속활주선 선형개발에 관한 연구)

  • Jeong, Uh-Cheul;Lee, Dong-Kun;Jung, Ki-Seok
    • Journal of Ocean Engineering and Technology
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    • v.30 no.2
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    • pp.69-74
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    • 2016
  • A new wave-piercing-type high-speed planing boat without a chine was developed, and its basic performance was investigated in a model test, including the resistance, trim, and sinkage. The maximum speed of the developed ship was 35 knots. The hull form was developed by combining a VSV (very slender vessel) and TH (transonic hull), which have large deadrise angles at the bow. The main dimensions were estimated by a statistical approach using actual ship data. The effect of a side fin attached at the stern near the water line was investigated from a resistance point of view. It was found that the developed hull form showed the possibility of a new concept for a high-speed planing hull without a chine, and the side fin played an important role in increasing the resistance performance by controlling the trim and sinkage in the high-speed range.

Nonlinear Potential Flow Analysis for the Hull with a Transom Stern (트랜섬 선미를 가지는 선형의 비선형 포텐셜 유동해석)

  • Choi, Hee-Jong;Lee, Gyoung-Woo;Chang, Yong-Chai
    • Journal of Navigation and Port Research
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    • v.30 no.8 s.114
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    • pp.631-636
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    • 2006
  • In this paper, the wave pattern around the hull with the transom stern advancing on the free surface with a constant speed was taken into consideration. To solve the problem the numerical analysis program was developed using Rankine source panel method based on potential flow analysis technique. The non-linearity of the free surface boundary conditions was fully satisfied. To verify the validity of the developed program the numerical calculations for Athena hull and KCS(KRISO container ship) hull was performed. The results of the numerical computation was compared with the ones of the model test experiment.

Experimental Evaluation for Damping Ratio Limit of Railway Bridge according to Structure Types (철도교량 구조형식별 감쇠비 하한값 산정을 위한 시험적 연구)

  • Min, Rak-Ki;Sung, Deok-Yong;Park, Yong-Gul
    • Journal of the Korean Society for Railway
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    • v.15 no.2
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    • pp.154-161
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    • 2012
  • The damping ratio of railway bridge has become one of the most important issues in dynamic design and dynamic stability of railway bridge. In the present study, laboratory and field test were performed for railway bridges such as a twin I-shaped steel composite girder, PSC box, steel box, PSC, IPC, PRECOM, preflex. The damping ratio of railway bridge according to structure types was estimated by logarithmic decrement method. Therefore, magnitude, frequency and amplitude of load did not affect damping ratio of railway bridge. Also, damping ratio limit of steel composite and PSC bridges was evaluated in 1.0%.

An Experimental Study on Magnus Characteristics of a Spinning Projectile at High Speed Region (회전발사체 마그너스 특성에 관한 고속 유동장 실험연구)

  • Oh, Se-Yoon;Lee, Do-Kwan;Kim, Sung-Cheol;Kim, Sang-Ho;Ahn, Seung-Ki
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.39 no.5
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    • pp.385-390
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    • 2011
  • The purpose of this research is to determine the dynamic Magnus effect data of a spinning projectile in wind-tunnel testing. In the present work, the high-speed wind-tunnel tests for the Magnus effect measurements were conducted on a 155-mm spin-stabilized projectile model in the Agency for Defense Development's Tri-Sonic Wind Tunnel at spin rates about 12,000 rpm. The test Mach numbers ranged from 0.7 to 2.0, and the angles of attack ranged from -4 to +10 deg. The validity of the wind-tunnel measurement techniques was evaluated by comparing them with the previous test results on the same configuration. The experimental results show that fair to good agreement is obtained with resonable accuracy.

Development of Magnus Effect Measurement Technique for Spinning Projectile (회전 발사체용 마그너스 효과 특정기법의 개발)

  • Oh, Se-Yoon;Kim, Sung-Cheol;Lee, Do-Kwan;Choi, Joon-Ho;Ahn, Seung-Ki
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.1
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    • pp.79-86
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    • 2007
  • The Magnus effect measurement apparatus was designed and built for spinning wind tunnel model which would simulate the rotation of projectiles. Prior to the high speed test, the ground functional test and the low speed test were carried out in the Agency for Defense Development's Low Speed Wind Tunnel(ADD-LSWT) at spin rates from about 6,000 to 10,000 rpm. Magnus force and moment were measured on the spinning projectile model at velocity of 100 m/s. It was shown that the Magnus force and moment were linear function of spin parameter. The test results were compared with Magnus test run on the same configuration in the Arnold Engineering Development Center's Propulsion Tunnel 4T(AEDC-4T).

Method of Test for Combustion Instability and Control at Model Combustor of Supersonic Engine (초음속 엔진 모델 연소기에서의 연소불안정 및 제어 시험 기법)

  • Choi, Ho-Jin;Hwang, Yong-Seok;Jin, You-In;Park, Ik-Soo;Yoon, Hyun-Gull;Kang, Sang-Hun;Lee, Yang-Ji
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.05a
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    • pp.111-115
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    • 2009
  • The method of test for observing the combustion instability and controling the instability actively by using secondary injection of fuel through flame stabilizer was studied by constructing model combustor of supersonic engine. The frequency of combustion instability was detected by measuring the pressure of combustor using pressure sensor and by optical sensing of flame intensity. Electro-magnetic valve was adopted as actuator for active control and the characteristics of modulated fuel was studied by measured pressure of valve outlet and scattering signal of spray at secondary fuel injection.

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