• 한국산학기술학회논문지
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• 제20권8호
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• pp.579-585
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• 2019

수중 표적의 탐지 효율을 증대시키기 위하여 능동 예인 음탐기는 적정 심도에서 바른 자세로 예인 되어야 한다. 본 연구에서는 능동 예인 음탐기의 꼬리 날개 형상이 예인 자세 및 예인 안정성에 미치는 영향을 확인하기 위하여 축소 모형 실험 2회 및 해상 실험 1회를 수행하고 그 결과를 분석하였다. 축소 모형 실험은 선형 수조에서 꼬리 날개 형상에 따른 속력 별 예인 거동을 측정하였으며, 축소 모형 실험에 활용된 꼬리 날개 형상은 I 형 꼬리 날개 1개와 Y 형 꼬리 날개 4개로 총 2종 5개에 대하여 실험을 수행하였다. 1차 축소 모형 실험에서는 Y형 꼬리 날개가 I 형 꼬리 날개 대비 예인 자세 및 예인 안정성이 우수함을 확인하였다. 2차 축소 모형 실험에서는 Y형 꼬리 날개를 기본으로 수직 꼬리 날개 높이 증가, 하부 수평 꼬리 날개 경사각 적용 형상에 대하여 속력 별 거동 특성을 확인하였으며, 하부 수평 꼬리 날개 경사각 적용 형상이 가장 우수한 성능을 나타내었다. 축소 모형 실험 결과를 검증하기 위해 실물 모형을 제작하여 해상 실험을 수행하였으며, 축소 모형 실험 결과와 유사함을 확인하였다.

• 대한조선학회논문집
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• 제44권2호
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• pp.55-63
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• 2007

Fins are widely used for roll stabilization of car ferries and passenger ships as well as high performance naval ships. In the present study, model experiments and numerical simulations are performed to investigate the influence of tail blades on the performance of a fin stabilizer for various angles of attack. It is found that a considerable improvement in performance of the fin stabilizer is achieved with adoption of the tail blades. The results can be utilized for the design of a high-lift control surfaces including fin stabilizers.

• 한국군사과학기술학회지
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• 제22권5호
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• pp.625-636
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• 2019

Recently, research on projectiles with wings for precision guidance is actively underway. In this study, we analyzed how the tail fins attached to the projectile affect the base drag. Aerodynamic analysis was performed with RANS(Reynolds Averaged Navier-Stokes) equations using FLUENT, a commercial CFD(Computational Fluid Dynamics) code. Through the aerodynamic analysis, the base drag characteristics of the projectile by parameters (number, length, thickness, position, shape of tail fin) were investigated. The results of this study are expected to be applicable to aerodynamic design of tail fins mounted on projectiles.

• Ocean Science Journal
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• 제41권4호
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• pp.201-205
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• 2006

Larval specimens of Halicampus punctatus were collected off Ulsan and Uljin in December 2002 (three specimens) and off Ulsan in December 2003 (one specimen). These specimens are characterized by the following morphological characteristics: rings, 14 + 35 = 49; subdorsal rings, 1 + 3 = 4; dorsal fin rays, 19 - 20; pectoral fin rays, 14 - 15; anal fm rays, 9; head length (HL), 5.8 - 6.7 in the standard length; snout length, 1.9 in HL; snout depth, 3.7 - 5.2 in snout length. The number of caudal fin rays 9 is less than those of the other species in the same genus 10. Wide stripe bands composed of small pigments are shown in the trunk and the tail. Melanophores are not found in the dorsal fin, the pectoral fin, and the anal fin except the caudal fin. The supraoccipital crest is on the head. The frontal ridge is on the dorsal side of front trunk. The blanched ridges on the opercular are fused with a main ridge like a tree branch. A few branched ridges that are small and narrow on the trunk and the tail are fused with the main ridges. We report these specimens as the first record in Korea and name them 'Byeol-sil-go-ki' in Korean.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2003년도 ICCAS
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• pp.537-541
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• 2003

In order to control the missiles by aerodynamics, control surfaces sometime called fins are used. Deflection angles of these fins are the right control variables of the aerodynamics, but aerodynamicists prefer to use analytic variables called aileron, elevator and rudder instead of these physical variables, because these three analytic variables dominantly influence on the roll, pitch and yaw channels of the missile maneuver, respectively, and each can be assumed a linear combination of four fin deflection angles. On that basis, roll, pitch and yaw autopilots for controlling the attitudes or lateral acceleration of the missile are designed, and as a consequence outputs of each autopilot are aileron, elevator and rudder commands, respectively. In the existing fin control scheme for the typical tail-fin controlled cruciform missiles, firstly these outputs are distributed to four fin defection commands, and after that four fins are actuated by fin controllers so that their deflections follow the commands. This paper shows that performance of such control schemes can be degraded significantly when fin actuators have certain physical constraints such as slew rate, voltage or current limit, uncertainty of actuator dynamics, and so on, and propose a new control scheme which alleviates such problems. This scheme can be widely applied to various fin actuation systems. But in this paper, for convenience, tail-fin controlled cruciform missile is taken as an example, and it is shown that a proposed control scheme gives better performance than the existing one.

• 한국군사과학기술학회지
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• 제25권1호
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• pp.45-54
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• 2022

There has been necessity to supplement the fin database to improve the accuracy of low-fidelity aerodynamic solver for missile configuration. In this study, fin database is expanded by in-house solver, utilized in the triservice data the previously established into regions beyond means of CFD. Fin alone data of CFD analysis results in the original region is matched well with triservice data originated from the wind tunnel tests. Extensive fin aerodynamic data from CFD analysis is added to the existing database of the low-fidelity solver. For confirmation, aerodynamic characteristics of body-tail and body-canard-tail missile configurations is computed using upgraded low-fidelity solver at transonic region. The result using improved solver shows good agreements with wind tunnel test and CFD analysis results, which implies that it becomes more accurate.

• 한국수산과학회지
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• 제42권6호
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• pp.725-728
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• 2009

Four specimens of Cynoglossus larvae (3.2-7.3 mm in notochord length, NL) collected from the middle Yellow Sea in August, 2008 were identified as Cynoglossus joyneri larvae based on morphological characteristics; (1) the two elongated dorsal fin rays on the parietal region, (2) protruded abdomen, (3) no melanophores on the mediolateral trunk and tail. Larva of 3.2 mm NL is compressed with a little big head and tapering, long tail. Larva of 7.0 mm NL has 115 dorsal fin and 85 anal fin rays, which are the same to those of adult. Larva of 7.3 mm NL tended to have concave part in the fringe of forehead, in which left-side eye may move to the other side.

• 한국발생생물학회지:발생과생식
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• 제21권2호
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• pp.193-204
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• 2017

The influence of triploidization on histological characteristics of retina, trunk kidney, liver and midgut tissue, and cell cycle of tail fin and gill tissue in far eastern catfish, Silurus asotus were analyzed. In the infertile triploid fish, the nucleus and/or cell size of secondary proximal tubule cells of trunk kidney, hepatocyte and midgut epithelium are much larger than those of the corresponding cells in the diploid fish (P<0.05). However, triploid tissue showed fewer number of outer nuclear layer in retina and nuclei in secondary proximal tubule of trunk kidney than those for diploid tissue. The mean percentages of the $G_l-$, the S- and the $G_2+M-phase$ fractions were 92.5%, 3.2% and 4.3% in tail fin tissue of diploid, and 93.4%, 2.6% and 4.0% in those of triploid, respectively. There were no significant differences in the percentages of each cell cycle fraction between diploid and triploid. The mean percentages of each phase fractions were 75.1%, 11.1% and 13.8% in gill tissue of diploid and 85.2%, 8.9% and 5.9% in those of triploid, respectively. The differences of cell cycle between tail fin tissue and gill tissue were statistically significant in diploid and triploid (P<0.05). Also, the differences between diploid and triploid were statistically significant in tail fin tissue and gill tissue (P<0.05). Cyclin D1 and cyclin E expressions were not significantly difference between gill tissue and tail fin tissue, and protein expressions of induced triploid were higher than those of diploid. Results from this study suggest that some characteristics in the triploid exhibiting larger cell and nucleus size with fewer number of cell than diploid can be used as an indicator in the identification of triploidization and ploidy level in far eastern catfish.

• Ocean and Polar Research
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• 제26권4호
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• pp.685-688
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• 2004

The morphology of the post-larva of Liopropoma japonicum of the family serranidae is described from one specimen collected off Jeju Island ($32^{\circ}42'N,\;127^{\circ}45'E$) on May 3, 2001. The body is laterally compressed and caudal peduncle deep at 19.4 mm BL. Anus locates at a vertical through posteriormost(8th) dorsal-fin spine. Dorsal fin rays were VIII, 14; anal fin rays III, 10; pectroal fin rays 16; pelvic fin rays I, 5. A caudal fin is rounded. Length of elongate second and third dorsal-fin spines are 499% and 423% of the body length, respectively. A series of 50 sensory pores on body is elongated to caudal fin. Head spination is well developed. Melanophores are moderately large and dense in the head, and are small and rare in teh neck. Being freshly collected, the body color is yellowish-red and tail is semitransparent. The head is yellowish-red and the brain is dark-red.

• 한국수산과학회지
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• 제8권4호
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• pp.225-233
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• 1975

1968년 6월,1969년 7월 및 1971년 7월에 해운대 동백섬 연안에서 채집된 953개체의 점망둑 자치어를 재료로 하여 초기생활사에 따른 형태변화 과정중 기조수의 변화, 색소포의 발달과정 및 배지느러미의 형성과정을 관찰하였다. 본 종은 제1등지내러미의 기조원기는 8.0 mm 전후에서 생겨나며 9.2mm 전후에서 완성하며 모든 지느러미의 연조는 초기치어기인 17.0mm 전후에서 완성된다고 생각된다. 색소포의 발달은 3단계로 구분할 수 있는데 후기자어기$(6.3\~14.2mm)$ 있어서 몸의 배면과 미부 복측면 및 꼬리지느러미 기저에 분포하고 있는 경우와, 후기 자어말기$(17.0\~2.44mm)$에 미부의 체측정중선에 일단의 색소총이 생기고 이것이 점점 전방으로 확대분포하는 시간 및 초기치어기$(27.2\~34.8mm)$에 몸 전체에 걸쳐 운형 및 H자상으로 분포되어 종의 특징을 나타내는 시기로 구분된다. 배지느러미의 형성과정은 후기자어기인 전장 7.4mm일 때 기조의 원기가 나타나서 17.0mm 전후에 기조가 완성되며 전장 30.0mm 전후에서 흡반이 완성된다.