• 한국수산과학회지
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• 제3권1호
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• pp.45-51
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• 1970

1926년~1967년의 42년간의 년간 총어획고를 자료로 하여 Periodogram 분석 방법에 의한 어황 보간과 어황 예측을 한 결과 다음을 얻었다.

• 해양환경안전학회지
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• 제26권2호
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• pp.195-205
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• 2020

동해 명태 서식처 환경은 한랭기와 온난기를 교차하며 변동을 지속하고 있다. 특히 1980년대 후반 이후 수온은 급격히 상승하였으며, 2000년대 후반 이후 다시 하강하는 특성을 나타내었다. 반면, 명태 주요 산란장이 위치한 동한만과 어장 중심이 형성되는 동해 중부 연안의 수온은 서로 다른 변동 특성을 나타내었다. 동한만의 겨울철 수온은 1980년 후반 이후 급격히 상승하였으며, 2000년 후반 이후 다시 하강하는 특성을 나타내었으며, 이러한 장기 변동특성은 2월과 3월에 더욱 뚜렷하였다. 반면 어장의 중심이 형성되는 동해 중부 연안의 수온은 1990년대 중후반 이후 지속적으로 상승하였으며, 2000년 후반 이후 수온이 하강하는 특성은 뚜렷이 나타나지 않았다. 이러한 산란장과 어장의 수온변화는 명태 자원량과 변동 특성이 유사하였다. 특히 산란장의 수온 변화는 난과 자·치어를 포함한 초기 생활사 시기의 생존율에 영향을 미치는 주요 인자로 작용한다. 1980년대에는 명태의 산란에 적합한 환경이 조성되는 면적과 지속시간이 평년보다 증가하였으며, 반대로 동해에 서식하는 명태의 자원량이 급격히 감소한 1980년대 후반 이후에는 산란장 면적과 적합한 환경이 지속되는 시간이 급격히 감소하였다. 명태 자원량 변화는 서식처의 물리적 환경변화와 유의한 상관성을 가지며, 특히 산란장의 수온 상승에 따른 산란에 적합한 환경이 조성되는 면적과 지속시간의 감소 그리고 어장의 축소는 명태 자원량 변화에 영향을 미치는 주요 인자로 작용하였다.

• 한국어류학회지
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• 제20권3호
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• pp.190-197
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• 2008

우리나라 남해안에서 멸치의 주 산란기인 2007년 5월부터 8월까지 멸치 난자치어의 분포와 해양환경요인과의 관계를 분석하고, 권현망에 의한 해역별 어획량과 체장조성 자료와 종합하여 멸치의 시공간 분포 변화를 분석하였다. 1. 멸치의 난은 5월부터 8월까지 분포하였으나, 분포밀도는 7월에 가장 높고 8월에 가장 낮았다. 2. 난의 주 분포해역은 남해도와 거제도 간 해역이며, 난이 많이 채집된 곳의 수온범위는 $15{\sim}24^{\circ}C$, 그리고 염분범위는 32~34이었다. 3. 멸치의 자치어의 분포밀도는 난의 분포와 같이 남해도와 거제도 간 해역에서 높았다. 4. 고흥반도와 거제도 간 해역에서 권현망어업에 의한 2007년 멸치 어획량은 통영이 11,409톤, 마산이 4,137톤, 사천이 2,487톤, 그리고 여수가 4,411톤으로 대부분이 남해도와 거제도 사이 해역에서 어획되었다. 5. 고흥반도와 거제도 간 해역에서 권현망어업에 어획된 멸치는 3~4월에는 큰 멸치(4.6 cm 이상)가 많았고, 8월 이후에는 0.7 cm의 소형에서부터 13.0 cm의 대형 크기까지 분포하였다. 작은 멸치(4.6 cm 미만)는 연안측 가까이에서 많이 분포하였고, 큰 멸치(4.6 cm 이상)일수록 어장의 외해측에 분포하여 멸치는 내만측에서 어린 시기를 보내고 성장하면서 외해측으로 이동 확산해 나가는 것으로 볼 수 있다.

• 한국운동역학회지
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• 제31권4호
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• pp.276-282
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• 2021

Objective: To investigate effects of Fibular Repositioning Taping (FRT) on lower extremity joint stiffness and angle during drop-landing. Method: Twenty-eight participants (14 healthy, 14 with chronic ankle instability [CAI]) performed drop-landings from a 60 cm box; three were performed prior to tape application and three were performed post-FRT. Three-dimensional kinematic and kinetic data were collected using an infrared optical camera system (Vicon Motion Systems Ltd. Oxford, UK) and force-plate (AMTI, Watertown, MA). Joint stiffness and sagittal angle of the ankle, knee, and hip were analyzed. Results: The hip [Healthy: p<.05; M ± SD: 29.43 ± 11.27 (pre), 33.04 ± 12.03 (post); CAI: p<.05; M ± SD: 31.45 ± 9.70 (pre), 32.29 ± 9.85 (post)] and knee [Healthy: p<.05; M ± SD: 53.44 ± 8.09 (pre), 55.13 ± 8.36 (post); CAI: p<.05; M ± SD: 53.12 ± 8.35 (pre), 55.55 ± 9.81 (post)] joints demonstrated significant increases in sagittal angle after FRT. A significant decrease in joint angle was found at the ankle [Healthy: p<.05; M ± SD: 56.10 ± 3.71 (pre), 54.09 ± 4.31 (post); CAI: p<.05; M ± SD: 52.80 ± 6.04 (pre), 49.86 ± 10.08 (post)]. A significant decrease in hip [Healthy: p<.05; M ± SD: 1549.16 ± 517.53 (pre), 1272.48 ± 646.73 (post); CAI: p<.05; M ± SD: 1300.42 ± 595.55 (pre), 1158.27 ± 550.58 (post)] and knee [Healthy: p<.05; M ± SD: 270.12 ± 54.07 (pre), 239.13 ± 64.70 (post); CAI: p<.05; M ± SD: 241.58 ± 93.48 (pre), 214.63 ± 101.00 (post)] joint stiffness was found post-FRT application, while no difference was found at the ankle [Healthy: p>.05; M ± SD: 57.29 ± 17.04 (pre), 59.37 ± 18.30 (post); CAI: p>.05; M ± SD: 69.15 ± 17.63 (pre), 77.24 ± 35.05 (post)]. Conclusion FRT application decreased joint angle at the ankle without altering ankle joint stiffness. In contrast, decreased joint stiffness and increased joint angle was found at the hip and knee following FRT. Thus, participants utilize an altered shock absorption mechanism during drop-landings following FRT. When compared to previous research, the joint kinematics and stiffness of the lower extremity appear to be different following FRT versus traditional ankle taping.

• International Journal of Internet, Broadcasting and Communication
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• 제12권3호
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• pp.226-232
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• 2020

Repetition of landing with visual control in sports and training is common, yet it remains unknown how landing with visual control affects postural stability and lower limb kinetics. The purpose of this study was to test the hypothesis that landing with visual control will influence on lower limb control for intrinsic dynamic postural stability. Kinematics and kinetics variables were recorded automatically when all participants (n=10, mean age: 22.00±1.63 years, mean heights: 177.27±5.45 cm, mean mass: 73.36±2.80 kg) performed drop landings from 30 cm platform. Visual control showed higher medial-lateral force, peak vertical force, loading rate than visual information condition. This was resulted from more stiff leg and less time to peak vertical force in visual control condition. Leg stiffness may decrease due to increase of perturbation of vertical center of gravity, but landing strategy that decreases impulse force was shifted in visual control condition during drop landing. These mechanism explains why rate of injury increase.

• 한국전문물리치료학회지
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• 제11권4호
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• pp.1-6
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• 2004

The kinematics involved in different landing strategies may be related to the occurrence of trauma. Several sources suggest that the angle of knee extension on touchdown and impact with the ground determines the magnitude of the impact force and, indirectly, knee loading. This study compared the initial knee angle and maximum knee flexion angle at the instant of impact on drop-landings between healthy men and women. In this study, 60 participants (30 males, 30 females) dropped from a height of 43 cm. A digital camera and video motion analysis software were used to analyze the kinematic data. When landing, there was significant difference between the two groups ($15.67{\pm}6.05^{\circ}$ in male, $24.10{\pm}6.34^{\circ}$ in female) in the mean knee flexion angle. The range of knee flexion on landing ($44.06{\pm}10.97^{\circ}$ in male, $36.96{\pm}9.99^{\circ}$ in female) also differed significantly (p<.05). The greater knee flexion that was observed in the male subjects would be expected to decrease their risk of injury. Women land with smaller range of knee flexion than men and this might increase the likelihood of a knee injury.

• 한국국방경영분석학회지
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• 제2권1호
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• pp.163-176
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• 1976

The artillery fire is characterized by great damage that can be inflicted simultaneously to an area through concentrated firing. The field artillery guns used in R.O.K. Army are generally old. Thus high values of their velocity errors cause wide dispersion of shell landings. Therefore effects of the concentrated firing is lessened. In this paper a general model which considers all error factors involved in firing in general, is established first. Then from this a basic model which includes the errors involved in concentrated firing only, such as the ballistic error, velocity error, target density function, and damage function, is extracted. Among many weapon systems now in use a specific one called gun 'A' is selected and its concentration effects are measured through computer simulation. The results show that as the velocity error of a battery increases, its target coverage capability, i. e. concentration effect, decreases. Therefore the need arises for the field artillery commander to know beforehand characteristics, i.e. velocity errors, of the guns in his unit and also to carefully examine the problem of battery arrangement with the gun characteristics in mind in order to maximize the damage effects of his artillery unit.

• 한국국방경영분석학회지
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• 제2권1호
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• pp.177-184
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• 1976

As the organizational size of a military service or business increases and its management becomes complex, the success in its management depends less on static type of management but more on careful, dynamic type of management. In this thesis, an operations research technique is applied to the problems of determining optimal air traffic control rule and of optimal capacity of air base for a military air base. An airport runway is regarded as the service facility in a queueing mechanism, used by landing, low approach, and departing aircraft. The usual order of service gives priority different classes of aircraft such as landings, departures, and low approaches; here service disciplines are considered assigning priorities to different classes of aricraft grouped according to required runway time. Several such priority rules are compared by means of a steady-state queueing model with non-preemptive priorities. From the survey conducted for the thesis development, it was found that the flight pattern such as departure, law approach, and landing within a control zone, follows a Poisson distribution and the service time follows an Erlang distribution. In the problem of choosing the optimal air traffic control rule, the control rule of giving service priority to the aircraft with a minimum average waiting cost, regardless of flight patterns, was found to be the optimal one. Through a simulation with data collected at K-O O Air Base, the optimal take-off interval and the optimal capacity of aircraft to be employed were determined.

• 한국수산과학회지
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• 제44권4호
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• pp.397-402
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• 2011

We surveyed the bycatch and discard of the shrimp-pot fishery in Hokkaido, Japan, three times during the major fishing period in September 2005. The surveyed catches were analyzed to separate bycatch, discard, and landings. To analyze bycatch and discard, we randomly selected 2 shrimp pots from each of 7 sets, for a total of 14 pots per survey. The total bycatch and discards from the rest of the shrimp pots were also analyzed in each survey. The total catch averaged 12 species. Coonstripe and pink shrimp catches averaged 74.7 kg/haul and 12.7 kg/haul, respectively. The weight of the bycatch averaged 33.4 kg/haul. The bycatch consisted mainly of snail fishes(5.1%), brittle stars(5.0%), and short-spined sea urchins(4.1%). Our analysis showed that the ratio of discard was 0.38, the rate of the discard was 27.4%, and the discard per unit effort was 33.4 kg/haul. The Hokkaido shrimp-pot fishermen discarded all of the bycatch except shrimps. Hence, the weight of the bycatch was equal to the weight of the discard. Our results comprise preliminary data that can be used to find ways to reduce bycatch and discard in the shrimp-pot fishery.

• International Journal of Aeronautical and Space Sciences
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• 제15권3호
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• pp.335-343
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• 2014

An airbag is an important safety system and is well known as a safety system in cars during an accident. Airbag systems are also used as a shock absorber for UAVs to assist with rapid parachute landings. In this paper, the dynamics and gas dynamics of five airbag shapes, cylindrical, semi-cylindrical, cubic, and two truncated pyramids, were modelled and simulated under conditions of impact acceleration lower than $4m/s^2$ to avoid damage to the UAV. First, the responses of the present modelling were compared and validated against airbag test results under the same conditions. Second, for each airbag shape under the same conditions, the responses in terms of pressure, acceleration, and emerging velocity were investigated. Third, the performance of a pressure relief valve is compared with a fixed-area orifice implemented in the air bag. For each airbag shape under the same conditions, the optimum area of the fixed orifice was determined. By examining the response of pressure and acceleration of the airbag, the optimum shape of the airbag and the venting system is suggested.