• Title/Summary/Keyword: stress amplitude

Search Result 537, Processing Time 0.035 seconds

The Qualitative Evaluation of Seismic Characteristics using the KMA Seismological Bulletin (1978-2001) (기상청 지진관측보고(1978-2001)를 이용한 지진 특성의 정성적 평가)

  • 박동희;연관희;최원학;장천중
    • Proceedings of the Earthquake Engineering Society of Korea Conference
    • /
    • 2002.03a
    • /
    • pp.12-19
    • /
    • 2002
  • A high frequency level of Fourier amplitude relates with stress drop and seismic moment. When we can not use this relation owing to absence of digital earthquake data, stress drop and seismic moment can be determined from Peak Ground Velocity(PGV) and felt area. We have qualitatively evaluated the seismic characteristics using PGV, and Magnitude from the well determined felt area in seismological records of Korea(1978~2001) by Korea Meteorological Administration(KMA). Observed relations between felt area and magnitude in the Korean Peninsula are explained by attenuation(Q), and stress drops comparing with the previous researches on stress parameter. This results are preliminary work for the study of stress parameter using the relationship of high frequency lavel, PGV, and felt area.

  • PDF

Structural Analysis on Durability of Pedal (페달의 내구성에 대한 구조 해석)

  • Cho, Jae-Ung;Han, Moon-Sik
    • Journal of the Korean Society of Manufacturing Process Engineers
    • /
    • v.10 no.4
    • /
    • pp.88-95
    • /
    • 2011
  • In this study, the deformation, stress, vibration, fatigue life and the probability of damage are analyzed at the pedal applied by the force of 300N. The maximum stress at the lower of pedal is shown as 20.801MPa. And the maximum displacement is 0.85mm at the maximum response frequency as 3800Hz. Among the cases of nonuniform fatigue loads, 'SAE bracket history' with the severest change of load becomes most unstable but 'Sample history' becomes most stable. In case of 'Sample history' with the average stress of 0 to $-10^{5}MPa$ and the amplitude stress of 0 to $10^{5}MPa$, the possibility of maximum damage becomes 0.6%. This stress state can be shown with 5 times more than the damage possibility of 'SAE bracket history' or 'SAE transmission'. The structural result of this study can be effectively improved with the design of pedal by investigating durability against its damage.

A Study of Loadings of Neck Muscles when Bent Backward (위보기 작업 시 EMG를 이용한 목 근육의 부하 평가)

  • Lee, Kwan-Suk;Park, Ju-Won
    • Journal of the Korean Society of Safety
    • /
    • v.27 no.1
    • /
    • pp.111-116
    • /
    • 2012
  • Workers who work with his neck bent backward in the standing posture have often complained of their musculoskeletal stress. The objective of this study was to find how much stress there was for workers who worked with their neck bent backward. The subjective evaluation and electromyography(EMG) were used to check the level of the stress. It was found that all subjects felt extreme pain after working with the neck bent backward and alternating 1 minute work and 0.5 minute rest for 30 minutes. The EMG level(amplitude) of neck muscles increased 80 percent on the average and the center frequency of EMG shifted to the lower frequency level which indicated fatigue of neck muscles. Thus, the intervention of this musculoskeletal stress is strongly recommended.

Study on Structural Analysis of Front Axle (전방 차축의 구조해석에 관한 연구)

  • Han, Moon-Sik;Cho, Jae-Ung
    • Journal of the Korean Society of Manufacturing Process Engineers
    • /
    • v.10 no.5
    • /
    • pp.65-71
    • /
    • 2011
  • This study analyzes about front axle through the analyses of stress, fatigue and vibration. Maximum equivalent stress is shown with the frequency of 60Hz in case of the harmonic vibration analysis applied with force. Among the cases of nonuniform fatigue loads, 'SAE bracket history' with the severest change of load becomes most unstable but 'Sample history' becomes most stable. In case of 'Sample history' with the average stress of 0 to $-2{\times}10^5MPa$ and the amplitude stress of 0 to $-2{\times}10^5MPa$, the possibility of maximum damage becomes 3%. This stress state can be shown with 6 times more than the damage possibility of 'SAE Bracket history' or 'SAE transmission'. The structural result of this study can be effectively utilized with the design of front axle by investigating prevention and durability against its damage.

A Study on Fatigue Crack Growth Behavior of Steel Using AE (AE을 이용한 강의 피로균열전파 거동에 관한 연구)

  • Chung, K.Y.;Kim, S.J.;Kim, Y.S.;Oh, M.S.;Kim, Y.D.
    • Journal of Power System Engineering
    • /
    • v.5 no.2
    • /
    • pp.50-56
    • /
    • 2001
  • In this study, the effect of specimen thickness and stress ratio on fatigue crack growth in S45C steel was investigated. Acoustic emission was monitored during the fatigue crack growth test. Both crack closure and AE technique were used in assessing fatigue crack growth behavior. Constant amplitude loading tests were performed on CT type specimen with three different thicknesses and stress ratios. Crack closure was investigated to explain the influence of specimen thickness and stress ratio on the fatigue crack growth in the second growth region. The crack closure effect was decreased with specimen thickness and stress ratio.

  • PDF

Study on Structural Analysis of Flywheel under Rotary Power (회전력을 받는 플라이휠의 구조해석에 관한 연구)

  • Han, Moon-Sik;Cho, Jae-Ung
    • Journal of the Korean Society of Manufacturing Process Engineers
    • /
    • v.11 no.2
    • /
    • pp.137-143
    • /
    • 2012
  • This study analyzes flywheel through the analyses of stress, fatigue and vibration. Maximum equivalent stress is 15.271MPa at the mid round shape and maximum deformation is 0.02264mm at the outer teeth. Among the cases of nonuniform fatigue loads, 'SAE bracket history' with the severest change of load becomes most unstable but 'Sample history' becomes most stable. In case of 'Sample history' with the average stress of -$10^4$MPa and the amplitude stress of 1000 to 2900MPa, the possibility of maximum damage becomes 30%. This stress state can be 20 times greater than the damage possibility of 'SAE bracket history' or 'SAE transmission'. The range of natural frequencies becomes 200 to 820Hz and the values of these deformations are not more than 10mm. The structural result of this study can be effectively utilized with the design of flywheel by investigating prevention and durability against its damage.

Study on Fatigue Durability Analysis of Poclain Bucket (포크레인 버켓의 피로 내구성 해석에 대한 연구)

  • Han, Moon-Sik;Cho, Jae-Ung
    • Journal of the Korean Society of Manufacturing Process Engineers
    • /
    • v.12 no.2
    • /
    • pp.8-13
    • /
    • 2013
  • This study analyzes about poclain bucket through fatigue durability analysis. Maximum equivalent stress and total deformation are shown at the lower of bucket and edge part respectively. Among the cases of nonuniform fatigue loads, 'SAE bracket history' with the severest change of load becomes most unstable but 'Sample history' becomes most stable. In case of 'Sample history' with the average stress of -10000Pa to 5000MPa and the amplitude stress of 0 to 6000MPa, the possibility of maximum damage becomes 3%. This stress state can be shown with 5 or 6 times more than the damage possibility of 'SAE bracket history' or 'SAE transmission'. The structural result of this study can be effectively utilized with the design of poclain bucket by investigating prevention and durability against fatigue damage.

Study on Durability by Structural Analysis of Bulldozer (불도저의 구조해석에 의한 내구성 연구)

  • Han, Moon-Sik;Cho, Jae-Ung
    • Journal of the Korean Society of Manufacturing Technology Engineers
    • /
    • v.20 no.3
    • /
    • pp.239-244
    • /
    • 2011
  • This study analyzes the behaviors on stress, fatigue and vibration about bulldozer in operation. Maximum equivalent stress is shown with the frequency of 100 Hz in case of the harmonic vibration analysis applied with force. Among the cases of nonuniform fatigue loads, 'SAE bracket history' with the severest change of load becomes most unstable but 'Sample history' becomes most stable. In case of 'Sample history' with the average stress of 0 to -105MPa and the amplitude stress of 0 to $1.617{\times}105MPa$, the possibility of maximum damage becomes 3.23%. This stress state can be shown with 5 times more than the damage possibility of 'SAE bracket history' or 'SAE transmission'. The structural result of this study can be effectively utilized with the design of bulldozer by investigating prevention and durability against its damage.

Structural Analysis on Control Arm of Automobile under Nonuniform Fatigue Load (불규칙 피로 하중을 받는 자동차의 컨트롤 암의 구조 해석)

  • Cho, Jae-Ung
    • Journal of the Korean Society of Mechanical Technology
    • /
    • v.13 no.3
    • /
    • pp.87-92
    • /
    • 2011
  • This study analyzes structural stress and fatigue on control arm of automobile under nonuniform load. Maximum equivalent stress at bolt part is shown with 419.1MPa and the corner is deformed with maximum displacement of 1.1628mm. Among 3 cases of nonuniform fatigue loads applying on control arm, 'SAE bracket history' with the severest change of load becomes most unstable but 'Sample history' becomes most stable. In case of 'Sample history' with the average stress of $-10^5MPa$ to $10^5MPa$ and the amplitude stress of 0 MPa to $10^5MPa$, the possibility of maximum damage becomes 3%. This stress state can be shown with 6 times more than the damage possibility of 'SAE bracket history' or 'SAE transmission'. Safety and durability on automobile can be effectively improved by applying the fatigue analysis result on control arm.

Numerical analysis of stress wave of projectile impact composite laminate

  • Zhangxin Guo;Weijing Niu;Junjie Cui;Gin Boay Chai;Yongcun Li;Xiaodong Wu
    • Structural Engineering and Mechanics
    • /
    • v.87 no.2
    • /
    • pp.107-116
    • /
    • 2023
  • The three-dimensional Hashin criterion and user subroutine VUMAT were used to simulate the damage in the composite layer, and the secondary stress criterion was used to simulate the interlayer failure of the cohesive element of the bonding layer and the propagation characteristics under the layer. The results showed that when the shear stress wave (shear wave) propagates on the surface of the laminate, the stress wave attenuation along the fiber strength direction is small, and thus producing a large stress profile. When the compressive stress wave (longitudinal wave) is transmitted between the layers, it is reflected immediately instead of being transmitted immediately. This phenomenon occurs only when the energy has accumulated to a certain degree between the layers. The transmission of longitudinal waves is related to the thickness and the layer orientation. Along the symmetry across the thickness direction, the greater is the stress amplitude along the layer direction. Based on the detailed investigation on the impact on various laminated composites carried out in this paper, the propagation characteristics of stress waves, the damage and the destruction of laminates can be explained from the perspective of stress waves and a reasonable layering sequence of the composite can be designed against damage and failure from low velocity impact.