• Title/Summary/Keyword: Mode II test

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Performance of Geogrids for Retarding Reflection Crack of Asphalt Overlay Pavement (아스팔트 덧씌우기의 반사균열 지연을 위한 지오그리드의 적용성 연구)

  • Kim, Kwang-Woo;Doh, Young-Soo;Kim, Bun-Chang;Lee, Moon-Sup
    • International Journal of Highway Engineering
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    • v.7 no.2 s.24
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    • pp.1-12
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    • 2005
  • This study was conducted to evaluate effect of geogrid and fabric, which are used underneath the overlaid asphalt pavement for retarding reflection cracking by simulated laboratory test. In this study, an interlayer at the interface between old concrete pavement surface and overlaid asphalt mixture, and polymer-modifier were used as an effort of retarding reflection crack initiation and for strengthening mixture. Five products were used in preparation of asphalt concrete beam specimen which was tack coated on top of jointed concrete block. Simulated Mode I and II fracture test were conducted under wheel loading and results were compared among those products. From the test results, several material and reinforcement combinations were observed to have a significant retardation effect against reflection cracking. The most effectively strengthened pavement against reflection cracking was found to be the LDPE-modifier asphalt mixture with a grid reinforcement at the bottom.

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Design of shunt structure to avoide TE mode in PLS-II storage ring vacuum chamber

  • Ju, Yeong-Do;Ha, Tae-Gyun;Park, Seong-Ju;Park, Jong-Do
    • Proceedings of the Korean Vacuum Society Conference
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    • 2010.08a
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    • pp.42-42
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    • 2010
  • We, previously, proved that the noise in the vertical readback from some of beam position monitors (BPMs) in the vacuum chamber of Pohang Light Source (PLS) are caused by the transverse electric (TE) longitudinal harmonic resonances. Based on this analysis, we now design the shunt structure to remove the TE mode resonces near the BPMs operation frequency of 500 MHz in the storage ring vacuum chamber of PLS upgrade project (PLS-II). The simulation result and experimental test result will be presented.

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Tow waviness and anisotropy effects on Mode II fracture of triaxially woven composite

  • Al-Fasih, M.Y.;Kueh, A.B.H.;Abo Sabah, S.H.;Yahya, M.Y.
    • Steel and Composite Structures
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    • v.26 no.2
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    • pp.241-253
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    • 2018
  • Mode II fracture toughness, $K_{IIC}$, of single-ply triaxially woven fabric (TWF) composite due to tow waviness and anisotropy effects were numerically and experimentally studied. The numerical wavy beam network model with anisotropic material description denoted as TWF anisotropic was first validated with experimental Mode II fracture toughness test employing the modified compact tensile shear specimen configuration. 2D planar Kagome and TWF isotropic models were additionally constructed for various relative densities, crack lengths, and cell size parameters for examining effects due to tow waviness and anisotropy. $K_{IIC}$ generally increased with relative density, the inverse of cell size, and crack length. It was found that both the waviness and anisotropy of tow inflict a drop in $K_{IIC}$ of TWF. These effects were more adverse due to the waviness of tow compared to anisotropy.

Life Firing Test of 1 N-class Monopropellant Thruster Development Model -Part II: Pulse Mode Performance (1 N급 단일추진제 추력기 개발모델의 장기수명 연소시험 -Part II: 펄스모드 성능 특성)

  • Won, Su-Hee;Kim, Su-Kyum;Jun, Hyoung-Yoll;Lee, Jun-Hui;Park, Su-Hyang;Lee, Jae-Won
    • Journal of the Korean Society of Propulsion Engineers
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    • v.18 no.6
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    • pp.68-74
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    • 2014
  • During the life firing test of 1 N-class thruster development model, pulse mode performance and performance changes were examined. The deviation of pulse mode response time according to thruster feed pressure was relatively small and the resultant ignition delay, response time, tail-off time were 32-35 ms, 86-91 ms, 89-98 ms, respectively. For the stabilized pulse region the impulse bit revealed the outstanding reproducibility of 1.41, 1.32, 2.10% at $3{\sigma}$. During the life firing test, the impulse bit was decreased with limited amounts, therefore the pulse mode performance could be considered to be maintained. The thrust centroid was also maintained during the life firing test.

Evaluation of Mixed-mode Interlaminar Fracture Toughness of Carbon Fabric/Epoxy Composites for Tilting Train Carbody (틸팅차량용 탄소섬유직물/에폭시 복합재의 혼합모우드 층간파괴인성 평가)

  • Yun, Seong-Ho;Heo, Gwang-Su;O, Jin-O;Lee, Sang-Jin;Jeong, Jong-Cheol;Kim, Jeong-Seok
    • Proceedings of the Korean Society For Composite Materials Conference
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    • 2005.11a
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    • pp.256-259
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    • 2005
  • Mixed-mode interlaminar fracture toughness of carbon fabric/epoxy composites, which are applicable to tilting train carbody, was evaluated through the MMB (Mixed-mode bending) test. Specimens were made of CF3327 plain woven fabric with epoxy and a starter delamination at one end was made by inserting Teflon film with the thickness of 12.5 μ m. Mixed-mode interlaminar fracture test was conducted for 6 types of specimens with the mode II ratio of 20 ,35, 50, 65, 80, 90%. Also crack propagating behaviors and fractured surfaces were examined through an optical travelling scope and a scanning electron microscope, respectively.

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Measurement of rock fracture toughness under mode I, II & mixed-mode conditions by using disc-typed specimens (인장, 전단 및 혼합모드에서 디스크 시험편을 이용한 암석의 파괴인성 측정에 관한 연구)

  • 장수호;이정인
    • Tunnel and Underground Space
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    • v.9 no.4
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    • pp.315-327
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    • 1999
  • Rock fracture mechanics has been widely applied to blasting, hydraulic fracturing, rock slope and many other practical problems in rock engineering. But a measuring method for the fracture toughness of rock, one of the mort important parameters in fracture mechanics as an intrinsic property of rock, has not been yet well established. To obtain mode I rock fracture toughness, the more favorable disc-typed specimens such as CCNBD, SCB, chevron-notched SCB and BDT were used in this study. Rock fracture toughness under mixed-mode and mode II conditions was measured by using the STCA applied to the CCNBD specimen. Size effects such as specimen thickness, diameter and notch length on fracture toughness were investigated. From the mixed-mode results, fracture envelops were obtained by applying various regression curves. The mixed-mode results were also compared with three mixed-mode failure criteria. In each fracture toughness test, acoustic emission was measured to get the data for determining the load levels of different crack propagation patterns.

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Calculation and Comparison of Liquid Oxygen Filling System between the KSLV-I Flight Test Data and the Modeling of the KSLV-II Launch Complex (한국형발사체 발사대시스템 산화제공급계 충전 운용 설계의 검증을 위한 나로호 비행시험 실증 자료 분석)

  • Seo, Mansu;Lee, Jae Jun;Hong, Ilgu;Kang, Sunil
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.5
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    • pp.107-114
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    • 2018
  • Korea Space Launch Vehicle (KSLV)-I flight test data and the modified 1-dimensional steady state modeling data from the critical design results of the KSLV-II liquid oxygen filling system operation are compared to validate the reliability of critical design modeling. A comparison of major flow rates and pressure values between test data and calculation results are conducted. The relative errors relative to maximum total flow rate for each cooling, filling, and replenishment mode are determined within 6.7%. Calculated pressure values at the outlet of the pump and the inlet of flow control valves are within 5.1%. The pressure at the inlet of the launch vehicle for each operation mode are within the measured pressure range.

A Correction Method for Operating Mode Analysis of Gas Generator Cycle Liquid Propellant Rocket Engine (가스발생기 사이클 액체로켓엔진작동 모드 해석의 보정 방법)

  • Nam, Chang-Ho;Moon, Yoonwan;Park, Soon Young;Chung, Enhwan
    • Journal of the Korean Society of Propulsion Engineers
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    • v.22 no.6
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    • pp.104-110
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    • 2018
  • Operating mode analysis of a liquid propellant rocket engine(LRE) is a crucial tool through the development of an engine. The operating mode analysis of an engine based on a collection of the acceptance tests of components shows discrepancies when compared to the test results. We propose a correction method for performance parameters to develop an engine analysis model for the gas generator cycle of an LRE. In order to simulate engine behavior, the performance parameters for the analysis model are tuned based on the test results of the 75tf engine of KSLV-II.

Measurement of the mixed mode fracture strength of green sandstone using three-point bending specimens

  • Li, Yifan;Dong, Shiming;Pavier, Martyn J.
    • Geomechanics and Engineering
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    • v.20 no.1
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    • pp.9-18
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    • 2020
  • Three-point bending specimens have been used to investigate the mixed mode fracture of green sandstone. Dimensionless stress intensity factors and T-stresses were calculated first by using the finite element method for various crack lengths, crack angles and span to length ratios. It is shown that three-point bending specimens can provide the whole range of mode mixities from pure mode I to pure mode II, provided suitable values are chosen for the crack angle and span to length ratio. The fracture test results were also used to compare with predictions of different criteria. These comparisons show that modified criteria including the influence of the T-stress agree better with experiment than the conventional criteria but that no one criterion matches perfectly the test results.

The Mixed Mode Fracture Using Concrete Disk (콘크리트 디스크를 이용한 혼합모드 파괴)

  • 진치섭;김희성;정진호
    • Journal of the Korea Concrete Institute
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    • v.12 no.2
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    • pp.63-69
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    • 2000
  • This study investigates a new method of using a concrete disk to calculate stress intensity factor (SIF) for mixed mode cases. The results indicate that the disk method is more accurate than three point bending test (TPB) in obtaining correct SIF values for mixed mode fracture propagation. Stress intensity factors $K_{I}$ and $K_{II}$ are calculated using a center notched disk subjected to splitting load. The notch angle is calculated by finite element (FEM). Fracture toughness $K_\textsc{k}$ of the concrete is obtained from the load intensities at the initiation of crack propagation. According to the finite element analysis(FEA) and disk test, the results show that mode I and mixed mode cracks propagate toward the directions of crack face and loading point, respectively. The results from FEA with maximum stress theory compare well with the experimental date. Unlike TPB method where an accurate fracture toughness value is difficult to obtain due to the irregular shape of load deflection curve and delayed final crack propagation (following slow stable cracking). fracture toughness value is easily measured in the disk test from the crack initial load. Therefore, it is safe to conclude that disk method is more advantageous than TPB method in analyzing combined mode fracture problems.