• The KSFM Journal of Fluid Machinery
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• v.2 no.1 s.2
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• pp.81-87
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• 1999

This study presents the measurement techniques on the periodic fluctuating flow such as the discharge flow of a centrifugal impeller in an unstable operating region. During rotating stall, the flow at the exit of a centrifugal compressor impeller fluctuates periodically with a lower frequency than that of the blade passing. To observe the blade-to-blade flow characteristics during the rotating stall, the phases of all the sampled data sets should be adjusted to those of the reference signals with two processes, in these processes, DPLEAT (Double Phase-Locked Ensemble Averaging Technique) can be used. From these measurements and data processing techniques, the characteristics illustrated a blade-to-blade flow with high frequency, but also a periodic rotating stall flow with a low frequency at the centrifugal impeller exit which was clearly observed.

• Journal of the Korean Solar Energy Society
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• v.28 no.1
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• pp.25-32
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• 2008

Aeroelastic phenomena of a wind turbine include stall-induced vibrations and classical flutters. The classical flutter occurs due to coalescence between bending mode and torsion mode. It is typically the aeroelastic instability of an aircraft wing. Different from the classical flutter, the stall-induced vibration is the instability in lead-lag mode due to negative aerodynamic dampings. In the present study, the three degree of freedom aeroelastic model of a wind turbine blade is introduced to characterize and analyze its aeroelastic phenomena. The numerical results show that the aeroelastic stability of flap-lag motion is more unstable than that of flap-pitch motion and the aeroelastic characteristics of lead-lag motion can become unstable as wind speed increases.

• Korean Journal of Veterinary Research
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• v.35 no.3
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• pp.625-630
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• 1995

During the period from june 1994 to february 1995 influence of free stall with concrete floor on profile of blood chemistry and clinico-morphopathogenesis of foot disease on 266 cows were studied. The results obtained as follow. 1. No differences between value of blood chemistry in normal and lame cows with foot disease were observed. 2. 20.7% of the cows were clinically lame. 3. Prevalence of clinical digital disorders were investigated: hyperplasia interdigitalis(45.8%), pododermatitis circumscripta(22.4%), dermatitis interdigitalis(9.4%), erosio ungulae(5.9%), phlegmona interdigitalis(3.5%), pododermatitis septica traumatica(3.5%), dermatitis digitalis(2.4%), white line disease(2.4%), pododermatitis aseptica diffusa(2.4%), dermatitis verrucosa(1.2%), fissura ungulae(1.2%) 4. Most claw lesions were located on lateral hindclaws and interdigital space of hindclaws.

• Proceedings of the KIEE Conference
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• 2006.07d
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• pp.1953-1955
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• 2006

500[MW]급 대용량 보일러 통풍계통의 송풍기 맥동 감시 장치는 송풍기 이상 발생시 송풍기를 보호하기 위하여 정지시키는 기능을 한다. 그러나 송풍기 맥동 감시 장치의 빈번한 고장으로 신뢰성이 저하되고 운전에 영향을 미치므로 이것을 DCS 로직으로 구성하여 신뢰성을 향상시켰다.

• 유체기계공업학회:학술대회논문집
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• 2006.08a
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• pp.387-390
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• 2006

Numerical study has been conducted in two dimensions about a NACA0012 airfoil with an oscillating microflap on the surface. We show that this microflap is effective in controlling the unsteady stall at high angles of attack. We solve the compressible Navier-Stokes equations for the Reynolds numbers with an extensible chimera grid fitted to the oscillatory microflap. For turbulent calculation, we adopt the SST $k-{\omega}$ model. We investigate the parametric effect of angle of attacks, Reynolds number, and the location where the microflap is installed.

• 한국전산유체공학회:학술대회논문집
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• 2006.05a
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• pp.382-384
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• 2006

• Journal of the Korean Society for Aviation and Aeronautics
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• v.13 no.3
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• pp.97-109
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• 2005

A canard type aircraft, which has good wing stall and stall/spin-proof characteristics, is under development. The aircraft prototype has full-depth core sandwich type wing and fixed landing gear, and has been built for test flights. Newly developing aircraft will be equipped with retractable landing gear and conventional foam core sandwich laminate structures and multi-rib wings. In this study, we present the structural test procedure and result for aircraft Firefly.

• Journal of the korean veterinary medical association
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• v.38 no.10
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• pp.926-934
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• 2002

• 월간낙농육우
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• v.19 no.3 s.203
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• pp.112-114
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• 1999

• Journal of Animal Science and Technology
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• v.55 no.4
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• pp.325-330
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• 2013

Providing an adequate environment for horses is important to minimize the level of stress for domesticated horses. The objectives of this study were 1) to evaluate the effect of living conditions on stress level of horses, 2) to observe the effect of one month confinement on self-maintenance behavior and stereotypic behavior of horses. The experiment was conducted at National Institute of Animal Science, Equine Field Station (Seonghwan-eup, Korea). Horses were staying in the paddock prior to the experiment. On day 1, five horses were randomly selected and housed in metal fence panels stall. Six horses remained in the same paddock. The ratio of neutrophil to lymphocyte (on day 15) and cortisol (on day 1 and 29) from stalled horses were significantly higher than horses in the paddock. Duration or frequency of self-maintenance behaviors such as feeding, drinking, resting, walking was not significantly different between day 1 and day 29. However, the frequency of urination significantly decreased (p<0.05) on day 29 compared with day 1. The frequency of stereotypic behaviors was not different between day 1 and 29. Our data indicate that horses may be more stabled when they are staying in the paddock rather than staying in the stall, but the stress level of horses in the stall during one month confinement was not effective for horses to adapt stereotypic behavior. In conclusion, providing an adequate environment and stress-less horse management techniques can minimize the stress level of horses.