• 제목/요약/키워드: 후퇴 각

검색결과 77건 처리시간 0.024초

`93 포장산업의 결산과 `94 전망

  • 한국포장협회
    • The monthly packaging world
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    • 통권9호
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    • pp.70-77
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    • 1994
  • 일본포장관리사회는 93년도 일본 포장업계 10대 뉴스에서 자국 포장업계가 93년도 한 해 '미증유의 시련기' 였음을 제일 첫째로 꼽고 있다. 거품경제 붕괴 뒤의 경기 후퇴, 엔고 등 나름대로 이유가 있었겠지만 국내 포장업계 사정도 일본의 경우와 크게 다르지 않았을 것으로 사려된다. 구랍 16일 한국포장협회 회의실에서 각 부문의 관계자들이 참석한 가운데 열린 좌담회를 통해 93년도 국내 포장산업의 회고와 94년도 전망을 들어본다.

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Combustion Characteristics of CH4 Nonpremixed Flame with Recession Distance (메탄 비예혼합 화염의 후퇴거리에 따른 연소특성)

  • Kim, Jun-Hee;Ku, Kun-Woo;Hong, Jung-Goo;Lee, Choong-Won;Kim, In-Su;Cheong, In-Mo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • 제36권3호
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    • pp.285-291
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    • 2012
  • A lot of research on the stability of nonpremixed flames has focused on the fuel-nozzle and quarl geometries. Of the work carried out, only a small amount has focused on the stability of the nonpremixed flame according to the recession distance and air-nozzle geometry. Therefore, in this study, a coaxial-diffusion-type gas burner with a swirler is designed for the systematic investigation of the combustion characteristics of a $CH_4$ flame depending on the recession distance and secondary air-nozzle geometry. 1st air is flowed through the swirler, and 2nd air is flowed through each nozzle. It is shown that the secondary air velocity greatly influences the flame length and shape. There is an optimum recession distance for each nozzle for the best combustion efficiency. In this study, it is shown that the optimized recession distance is nearly half the outer diameter of the air-supply nozzle.

EVALUATION OF CONDYLAR DISPLACEMENT USING COMPUTER TOMOGRAPHY AFTER THE SURGICAL CORRECTION OF MANDIBULAR PROGNATHISM (전산화단층촬영법을 이용한 하악전돌증 환자의 외과적 악교정술후 하악과두 위치 변화 검토)

  • Lee, Ho-Kyung;Jang, Hyun-Jung;Lee, Sang-Han
    • Maxillofacial Plastic and Reconstructive Surgery
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    • 제20권3호
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    • pp.191-200
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    • 1998
  • This study was intended to perform the influence of condyle positional change after surgical correction of skeletal Class III malocclusion after orthognathic surgery in 37 patients(male 13, female 24) using computed tomogram that were taken in centric occlusion before, immediate after, and long term after surgery and lateral cephalogram that were taken in centric occlusion before, 7 days within the period of intermaxillary fixation, at the 24 hours later removing intermaxillary fixation and long term after surgery. 1. Mean intercondylar distance was $84.42{\pm}5.30mm$ and horizontal long axis of condylar angle was $12.79{\pm}4.92^{\circ}$ on the right, $13.53{\pm}5.56^{\circ}$ on the left side. Condylar lateral poles were located about 12mm and medial poles about 7mm away from the reference line(AA') on the axial tomogram. Mean intercondylar distance was $83.15{\pm}4.62mm$ and vertical axis angle of condylar angle was $76.28{\pm}428^{\circ}$ on the right, $78.30{\pm}3.79^{\circ}$ on the left. 2. In amount of set back, We found the condylar change(T2C-T1C) which had increasing tendency in group III (amount of setback : 10-15mm). but there was no statistical significance(p>0.05). 3. There was some correlation between condylar change(T2C-T1C) and TMJ dysfunction. It seemed that postoperative condylar change had influenced postoperative TMJ dysfunction, through there was no statistical significance (p>0.05). As we have observed the change of condylar axis in the group that complained of TMJ dysfunction in cases of large amount of mandibular setback. So we consider that the more trying to conserve condylar position will decrease occurrence rate of post operational TMJ dysfunction.

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The Study of Advanced Propeller Blade for Next Generation Turboprop Aircraft -Part I. Aerodynamic Design and Analysis (차세대 터보프롭 항공기용 최신 프로펠러 블레이드 연구 -Part I. 공력 설계 및 해석)

  • Choi, Won
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • 제40권12호
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    • pp.1017-1024
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    • 2012
  • The aerodynamic design and analysis on advanced propeller with blade sweep was performed for recent turboprop aircraft. HS1 airfoil series are selected as a advanced propeller blade airfoil. Adkins method is used for aerodynamic design and performance analysis with respect to the design point. Adkins method is based on the vortex-blade element theory which design the propeller to satisfy the condition for minimum energy loss. Propeller geometry is generated by varying chord length and pitch angle at design point of target aircraft. Advanced propeller is designed by apply the modified chord length, the tip sweep which is based on the geometry of conventional propeller. The aerodynamic characteristics of the designed Advanced propeller were verified by CFD(Computational Fluid Dynamic) and evaluated to be properly designed.

Reliability Analysis of Stability of Berm Breakwaters (소단형 방파제의 안정성에 대한 신뢰성 해석)

  • Lee, Cheol-Eung
    • Journal of Korean Society of Coastal and Ocean Engineers
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    • 제19권5호
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    • pp.399-407
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    • 2007
  • Two reliability models, AFDA(Approximate Full Distribution Approach) and Monte-Carlo simulation method, are directly developed to study on both hydraulic failure mode of berm recession and structural failure mode of armour breakage of berm breakwaters. By comparing the present results with the results of other researcher, it may be confirmed that two reliability models can be straightforwardly applicable to berm breakwaters. Relative influence of each random variable on hydraulic and structural failure probabilities could be properly analyzed. The upper bound and the lower bound of failure probability can be evaluated by using bi-modal bounds of the multiple failure mode analysis, from which it may be possible to investigate some kinds of dependence into between two failure modes. Finally, it may also be found that the structural failure mode of armour breakage could become a main failure mode of berm breakwaters in the condition of more than any allowable berm recession.

The effects of mandibular setback osteotomy on the oropharyngeal airway space in mandibular prognathic patients (하악전돌 환자에서 하악골 후퇴수술이 기도공간에 미치는 영향)

  • Kim, Hyo-Young;Choi, Hyun-Gue;Kim, Eun-Kyung;Kim, Jong-Ghee
    • The korean journal of orthodontics
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    • 제27권5호
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    • pp.733-741
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    • 1997
  • As a result of surgical orthodontic treatment of mandibular prognathism, changes take place in the skeletal and soft orofacial components. Although some investigators had stated that permanent reduction of airway space was observed after mandibular setback surgery, it was not clear that this permanent reduction was sustained during long-term follow-up. The purpose of this study was to assess the changes in oropharyngeal airway space and soft tissue orofacial component following the mandibular setback surgery and during the follow-up period. The correlation between the changes of the oropharyngeal airway space and the changes of other soft tissue orofacial component was also assessed. The findings of this study were as follows ; 1. The oropharyngeal airway space area decreased following mandibular setback surgery for mandibular prognathism and continued to decrease during the follow-up period(p<0.05). 2. The pharyngeal depth at Xi point level and the 2nd cervical vertebra point level decreased after the surgery and remained during the follow-up period(p<0.05). The decrease of these pharyngeal depth was correlated with the decrease of oropharyngeal airway space area(p<0.01). 3. The decrease of pharyngeal depth at the 3rd and 4th cervical vertebra point level was not significant after the surgery and during the follow up period. 4. The hyoid bone moved downward after the surgery(p<0.05), but returned to its original position during the follow-up period. 5. The length & height of tongue and the Position of epiglottis base did not change significantly(p>0.05). 6. The soft palate was displaced posteriorly after the surgery and remained to its changed position during the follow-up period(p<0.05) due to posterior displacement of tongue. The changes of soft palate were significantly correlated with the decrease of oropharyngeal airway space area(p<0.01). 7. The narrowing of oropharyngeal airway space was due to the posterior displacement of tongue above the level of epiglottis tip. The posterior displacement of tongue following mandibular setback osteotomy remained during the follow-up period.

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Evaluation of Shoreline Retreat Rate due to a Sea Level Rise using Theory of Equilibrium Beach Profile (평형해빈단면이론을 이용한 해수면 상승에 따른 해안후퇴율 산정)

  • Kang, Tae Soon;Cho, Kwangwoo;Lee, Jong Sup;Park, Won Kyung
    • Journal of Korean Society of Coastal and Ocean Engineers
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    • 제26권4호
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    • pp.197-206
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    • 2014
  • The purpose of this study is to evaluate coastal erosion due to a sea-level rise. The shoreline retreat rate was calculated due to future sea-level rise. Shoreline retreat rates were quantified with the cross-sectional data of 23 sandy coasts (12 sites from east coast, 5 sites from south coast, and 6 sites of west coast) and 3 cross-sectional profiles from each side of the coasts in Korea. The theory of equilibrium beach profile was employed in this study to evaluate the applicability of the theory into the coast of Korea and was tested with 15 cross-sectional beach profiles. Four scenarios of future sea level rise such as 38 cm, 59 cm, 75 cm, and 100 cm were adopted to estimate the shoreline retreat rates. Overall shoreline retreat rates for the coasts in Korea were predicted as 43.7% for 38 cm, 60.3% for 59 cm, 69.2% for 75 cm, and 80.1% for 100 cm sea level rises, respectively. Retreat rates in the east coast (29.6% for 38 cm, 45.1% for 59 cm, 56.0% for 75 cm, and 69.9% for 100 cm) showed relatively low compared to the south coast (51.9%, 67.6%, 77.2%, 87.3%) and the west coast (53.8%, 71.0%, 78.5%, 86.4%). However, all sandy coasts in Korea were assessed to be vulnerable with increasing sea-level rise. There are uncertainties in the assessment of this study, which include the limitation of the assessment model and the lack of the spatio-temporal data of the beach profiles. Therefore, this study shows that it is very important to spend integrated efforts to respond coastal erosion including comprehensive observations(monitoring) and the development of scientific understanding on the field.

Petrogenesis of the Orbicular Gneiss in the Muju area (무주 구상편마암의 성인에 관한 연구)

  • 김용완;김형식;이설경
    • The Journal of the Petrological Society of Korea
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    • 제4권2호
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    • pp.186-200
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    • 1995
  • 구상구조를 보이는무주 구상편마암은 전북 무주군 왕정리일대에 분포하는 정편마암인 함전기석 복운모 화강편마암내에 배태되어 있다. 구상구조는 구상편마암의 기원암인 화강암내에 포획된 이질암이 변성분화작용을 받아 생성된 것으로 사료된다. 구상편마암은 각의 발달이 없는 초생암구로 구성된 TypeI의 암구와 각의 발딜이 있는 TypeII로 구분이 가능하다. TypeII는 단각암구와 다각암구 그리고 핵의 구조에 따라 다양한 형태로 나눌수 이TEk. 구성암은 내핵, 외학, 각, 그리고 기질부로 구성된다. 핵의 장경은 보통 5cm 내지 8cm이며 구형 또는 타원형의 행태로 암구으 중심부를 이루고 있다. 핵의 화학성분은 $Al_2O_3$, total $Fe_2O_3$, MgO, $K_2O$ LREE가 풍부하고 반대로 $Na_2O$, CaO, HREE가 결정된 것이 특징이며, 핵을 주로 구성하는 변성광물은 근청석-규선석-흑운모-올리고클레이스이다. 각은 운모류의 우혹질 각과 장석류의 우백질 각으로 구분되며 수mm내지 수cm의 두께를 이루며 단일각 내지 다각구조를 이루고 있다. 이들은 핵에 비하여 $Na_2O$, CaO가 상대적으로 부화되고 있으며 기질부를 이루는 화강편마암의 조성과 유사하다. 기지루는 반상변정질로 되어 있고 장석 반상변정의 크기는 대략 2내지 3 mm의 크기로 구성되어 있으며 부수적으로 운모류와 소량의 전기석과 규선석이 존재한다. 또한 후기에 유입된 많은 유체들에 의한 후퇴변성작용의 영향으로 장석은 견운모화내지 전기석화되고, 근청석은 피나이트화 되었다.

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Effects of Strake Planform on the Vortex Flow of a Double-Delta Wing (이중 삼각날개의 와류에 미치는 스트레이크 평면형상의 영향)

  • 손명환;정형석
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • 제34권8호
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    • pp.16-23
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    • 2006
  • The effects of strake planform shapes on the vortex formation, interaction, and breakdown characteristics of double-delta wings were investigated through pressure measurements of upper wing surface and off-surface flow visualization. Three different shapes of strakes were attached to a delta wing respectively to form double-delta wing configurations and tested in a medium-sized subsonic wind tunnel. The results of the pressure measurements indicated that the strake planform having a higher sweep angle generated more concentrated vortex systems at upstream locations, which, however, tended to diffuse and break down much faster at the downstream locations. It was also found from the off-surface visualization results that the cause for the vortex concentration was due to the acceleration of coiling and merging processes between the wing and strake vortices.

A Study on Spray Angle of Dual Swirl Injector with Different Recess Length (Dual Swirl Injector Recess 길이에 따른 분산각 평가)

  • Park, Hee-Ho;Kim, Tae-Han;Kim, Yoo
    • Journal of the Korean Society of Propulsion Engineers
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    • 제7권3호
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    • pp.30-37
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    • 2003
  • Spray angle of dual swirl injector is established according to the velocity ratio at orifice exit. Due to the internal mixing at recess and lack of correlation for the combined two fluid injection, prediction of spray angle is very difficult. This study deal with experimental work and numerical simulation on spray angle with different recess length. Among the multiphase flow models, the VOF model was selected to simulate the spray angle. Feasibility of numerical analysis are confirmed by comparing the results with the experimental data, and the effect of recess on spray angle are analyzed for single and combined spray case.