• Title/Summary/Keyword: 후퇴 길이

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A Study on the Local Regression Rate of Solid Fuel in Hybrid Rocket (하이브리드 로켓에서의 고체연료의 국부 후퇴율에 관한 연구)

  • Lee, Jung-Pyo;Kim, Gi-Hun;Cho, Jung-Tae;Kim, Soo-Jong;Moon, Hee-Jang;Sung, Hong-Gye;Kim, Jin-Kon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.05a
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    • pp.89-92
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    • 2008
  • In generally, the regression rate equation was only expressed by function of oxidizer massflux in hybrid propulsion system. This can not represent the local value of regression rate along with oxidizer flow direction. In this study, experimental studies were performed with several pieces of solid fuel. As results, the local regression rate decreases rapidly with axial location near entrance, and increases with axial distance from the leading edge. The empirical formula for local regression rate with function of oxidizer massflux and length was derived.

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A Study on Combustion Characteristics of Hybrid Rocket with the Variation of L/D Ratio (하이브리드 로켓의 L/D 비 변화에 따른 연소특성 연구)

  • Kim Soo-Jong;Kim Jin-Kon;Lee Seung-Chul;You Woo-Jun;Lee Jung-Pyo
    • Journal of the Korean Society of Propulsion Engineers
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    • v.9 no.4
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    • pp.31-38
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    • 2005
  • In this paper, the combustion characteristics of a hybrid propulsion system were studied with various L/D(length vs diameter) ratio of the single po.1 type solid fuel. Experiments were performed for 2 cases with the fixed grain port diameter and fuel length respectively. For the first case, results show that there are no large variations for regression rates as the L/D ratio changes. And as the L/D ratio increases, the O/F ratio decreases and thrust, characteristic velocity tends to increase. For the second case, there is no large change for O/F ratio, thrust and characteristic velocity as L/D ratio changes. On the other hand, as the L/D ratio decreases, only the regression rate tends to increase. Experimentally, exponent n in $\dot{r}=a{G_0}^n$ was found about 0.5 and then the O/F ratio was shown nearly constant. In the experiment, PE and gas oxygen were used as a fuel and an oxidizer.

Granulite xenoliths in porphyroblastic gneiss from Mt. Jiri area, SW Sobaegsan massif, Korea (소백산육괴 서남부 지리산지역의 반상변정질 편마암에서 산출되는 백립암질 포획암)

    • The Journal of the Petrological Society of Korea
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    • v.8 no.1
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    • pp.34-45
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    • 1999
  • Mafic granulite xenoliths are found in precambrian porphyroblastic gneiss of the Mt. Jiri area, SW Sobaegsan massif, Korea. The xenoliths are rounded to ellipsoidal in shape, 50-100 cm in length and coarse-grained with granoblastic and foliated texture. The xenoliths consist of orthopyroxene, garnet, biotite, plagioclase, quartz, ilmenite and secondary orthoamphibole. Orthopyroxene is mostly resorbed and rimmed by coronitic orthoamphiboles. Garnets occur as porphyblasts and are zoned with higher pyrope content in cores than in rims. Geothermo-barometry results yield conditions of about $800-850^{\circ}C$, 6 kb and $500^{\circ}C$, 4 kb for early and retrograde stages of equilibration, respectively. According to available geochronological data, it is suggested that the granulite facies metamorphism occurred prior to 2.1-1.9Ga and that the area was superimposed by the high-grade (over $600-700^{\circ}C$) metamorphism between 1.9-1.7Ga, followed by cooling during uplift.

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천리길을 걸어갈 수 없다 - 과학문명 외면한 무공해농산물 주장

  • 한국농약공업협회
    • The Bimonthly Magazine for Agrochemicals and Plant Protection
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    • v.7 no.6
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    • pp.11-20
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    • 1986
  • 최근 각종 언론매체나 소비자단체에 의해 과장되고 있는 무공해농산물 주장은 수확량감소 및 위화감조성등 득보다는 실이 많은 과학의 후퇴를 의미한다 할 수 있다. 일반농산물은 과연 오염됐는가? 아니면 무공해 농산물이란 용어자체가 공해란 말에 민감하게 반응하는 맹점을 이용한 유명무실한 허상은 아닌지 살펴보도록 한다.

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병아리 세일즈맨의 노오트(2) -내가 발딛고 있는 양계업계

  • 이중길
    • KOREAN POULTRY JOURNAL
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    • v.6 no.10 s.60
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    • pp.82-85
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    • 1974
  • $\ulcorner$세일즈에 있어서 인격이란 최대이면서 최종의 힘이 되리라 확신한다. 무엇보다도 성실과 근면을 바탕으로 꾸준히 노력하는 자세가 절대로 필요로 하는 것이다 하겠다.$\lrcorner$ 금년같이 그 어느때 보다도 심각한 경기후퇴와 어두운 경기전망 가운데 여하히 불꽃튀는 판매전선을 뚫고나갈 것인가? 필자는 세일즈맨으로서 인간적인 성실과 근면을, 그리고 보다 정확한 정보판단을 할 수 있어야 한다고 강조한다.

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A Study on Combustion Characteristics of Hybrid Rocket with the Variation of L/D ratio (하이브리드 로켓의 L/D 비 변화에 따른 연소특성 연구)

  • Kim Soo-jong;Kim Jin-kon;Lee Seung-chul;You Woo-jun;Lee Jung-pyo
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • v.y2005m4
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    • pp.83-87
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    • 2005
  • In this paper, the combustion characteristics of a hybrid propulsion system were studied with various L/D(length vs diameter) ratio of the single port type solid fuel. Experiments of L/D ratio change were performed for 2 cases with the fixed grain port diameter and fuel length respectively. For the First case, results show that there are no large variation for regression rates as the L/D ratio changes. And as the L/D ratio increases, the O/F ratio and thrust tends to increase. For the Second case, there are no large change for O/F ratio and thrust as L/D ratio changes. On the other hand, as the L/D ratio decreases, only the regression rate tends to increase.

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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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    • v.40 no.12
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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.

A Study on the Erosion and Retreat of Sea-Cliff through the Multi-temporal Aerial Photograph Data and Field Survey: The Case Study of Taean Peninsula, Korea (다중시기 항공사진과 현장조사를 통한 해안침식 변화 연구: 태안반도를 사례로)

  • WOO, Han-byol;JANG, Dong-Ho
    • Journal of The Geomorphological Association of Korea
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    • v.17 no.4
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    • pp.71-83
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    • 2010
  • In this study, the volume of shoreline retreat at sea-cliffs in the Taean peninsula(West Coast of Korea) was estimated and their erosion and seasonal landforms characteristics changes were investigated through multi-temporal aerial photographs and field survey. Based on the analysis of aerial photographs through ortho-correction, the results show that the length of shoreline and erosion area increase as erosion at sea-cliffs occurs in Pado-li and Dundu-li. To obtain the seasonal quantitative landforms changes and retreat of sea-cliffs, we marked top, middle, and bottom datum-points, from which the distance to the nearest bedrock was repeatedly measured. In these regions, the retreat of sea-cliffs gradually increases in spring to summer, but gradually decreases in autumn. In particular, the typhoon that has a great influence on the Korean peninsula in July to September in summer would drastically increase the retreat of sea-cliffs in comparison with other seasons. As the outcrop of sea-cliffs repeats freezing and thawing in winter, the retreat of sea-cliffs increases a little due to active mechanical weathering. To know the erosion and seasonal landforms changes of sea-cliffs, we took pictures of them in every month and then analyze their condition. The retreat of sea-cliffs was repeatedly occurred by the circulation of the erosion of sea-cliff base, landslides, the formation of slope sediment debris and their erosion, in that order.

A CROSS-SECTIONAL LONGITUDINAL CEPHALOMETRIC STUDY ON CRANIOFACIAL SKELETAL CHARACTERISTICS IN KOREAN CHILDREN AGED 6 TO 14 WITH CLASS III MALOCCLUSIONS (III급 부정교합을 지닌 $6\sim14$세 아동의 중두개저각에 따른 안면두개골의 형태적 특징: 측두방사선규격사진을 이용한 횡단누년적 연구)

  • Park, Soo-Bae;Choi, Yeong-Chul
    • Journal of the korean academy of Pediatric Dentistry
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    • v.27 no.1
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    • pp.135-145
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    • 2000
  • It is well known that there are different craniofacial skeletal groups in the same malocclusion types. The present study was performed to determine morphologic sub-groups in Korean children with Class III malocclusions, and to find out morphological differences between subgroups by means of a cross-sectional longitudinal cephalometric study. In this study, 135 children aged 6 to 14 year-old with untreated Class III malocclusions were selected. The samples were divided into two groups depending on the angulation of middle cranial fossa (MCF). That is, when the MCF of an individual was measured smaller than 40.3, he/she was tossed into mandibular protrusive-effect group(MREG), while when an individual was measured larger than 40.3, he/she was tossed into mandibular retrusive-effect group(MREG). Thereafter, the grouped samples were divided into 4 age groups(7, 9, 11 and 13 year-old). Thirty four linear and angular measurements on the tracings of lateral cephaloradiographs were measured, and the morphological characteristics and differences were compared and analysed by means of Wilcoxon test. It was found that Korean children with Class III malocclusions were divided into two groups, in which 39.3% were belonged in the MREG and 60.7% were in the MREG. In the MREG, anterior-posterior length of cranial base, nasomaxillary complex, maxilla and mandible were larger than the MREG. And although there was no difference in the total length of mandible (Co-Gn), mandibular body length (Go-Gn) was larger in the MREG during the majority of the observed periods. These results would suggest that a majority of the samples, 60.7%, demonstrated many of configurations of craniofacial skeletal relationships that can be found in the leptoprosopic faceform.

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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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    • v.7 no.3
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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.