• 제목/요약/키워드: Preliminary-Design

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Preliminary Design and Analysis of the Small-scale Hybrid Rocket Motor (소형 하이브리드 로켓 모터 기초 설계 및 해석)

  • Kim, Sun-Kyoung;Cho, Min-Kyung;Yoon, Chang-Jin;Kim, Jin-Kon;Sung, Hong-Gye;Moon, Hee-Jang
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.11a
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    • pp.415-418
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    • 2006
  • 하이브리드 추진제는 연소 중 연료의 후퇴율 및 연소 면적의 변화로 인해 O/F비가 변화하므로 이로 인해 설계 및 해석에 어려움을 가지게 된다. 본 연구에서는 요구임무를 만족하는 하이브리드 로켓모터에 대한 설계를 수행하였다. 하이브리드 모터의 기초 설계를 실시하고 그 결과를 이용하여, 일정한 산화제 유량이 공급된다는 가정 하에, 연소 시 연소면적변화에 따른 O/F비 변화를 고려한 하이브리드 모터의 내탄도 해석을 실시하였으며, 그 결과를 이용하여 로켓의 외탄도 해석을 실시하였다.

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Performance Analysis of the Centrifugal Pump Impeller Using Commercial CFD Code (상용 CFD코드를 이용한 원심펌프 임펠러의 성능해석)

  • Choi, Young-Seok;Lee, Yong-Kab;Hong, Soon-Sam;Kang, Shin-Hyung
    • 유체기계공업학회:학술대회논문집
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    • 2000.12a
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    • pp.305-311
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    • 2000
  • A commercial CFD code is used to compute the 3-D viscous flow field within the impeller o( a centrifugal pump. Several preliminary numerical calculations are carried out to determine the influence of the parameters such as the grid systems, the numerical schemes, the turbulence models and the shape of the vaneless diffusers at the design flow rate. The results of the preliminary study are used for the calculation of the off-design flow conditions. The circumferentially averaged results such as the radial and tangential velocities, the exit flow angle, the slip factor, the static pressure and the total pressure are compared with the experimental data at the impeller exit to discuss the influence of the prescribed parameters.

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NUMERICAL STUDY ON WIND TUNNEL GROUND PLATE WITH A PRESSURE CONTROL DEVICE (압력 조절 장치를 갖는 풍동 지면판에 관한 수치해석적 연구)

  • Lee, M.J.;Kim, C.W.
    • Journal of computational fluids engineering
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    • v.15 no.4
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    • pp.53-59
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    • 2010
  • Preliminary design of a ground plate, a device installed close to the aircraft model for wind tunnel test to simulate the ground effect, was performed by a numerical simulation. A two-dimensional numerical study was performed initially to decide the optimal leading edge and flap configurations. Then, three-dimensional studies were conducted to decide the optimal flap deflection angle for pressure distribution reduction since the plate and the plate supporting system generate static pressure difference between the upper and lower flow regions. Three-dimensional simulation additionally studied the effect of the clearance between the plate and the wind tunnel side wall. For the efficiency of computation, half model was simulated and a symmetric boundary condition was applied on the center plane. Based on the preliminary design, a ground plate was designed, manufactured and tested at the Korea Aerospace Research Institute(KARI) wind tunnel. The measured pressure differences versus flap deflection angle agreed well with the predicted results.

Vibration Analysis of [αββγααβ]r Type Laminated Composite Plates Using Invariant and Correction Factor (불변량(不變量)과 수정계수(修正係數)를 사용(使用)한 [αββγααβ]r 적층부합판(積層復合板)의 진동해석(振動解析))

  • Hong, Chang-Woo;Sim, Do-Sik;Kim, Nam-Yun;Jung, Young-Hwa
    • Journal of Industrial Technology
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    • v.16
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    • pp.131-137
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    • 1996
  • For a large scale civil and architectural structures, mainly steel, concrete and aluminum have been used and weight and corrosion of materials became a major concern. Designing with composite materials is very much complicated. Simple classical theory may yield good results for selecting "initial" sections for preliminary design. D. H. Kim proposed to use the quasi-isotropic constants by Tsai for the preliminary design of the composite primary structures for the civil construction. Also he made simple equation using correction factor. In this paper, the simple formulas developed by D. H. Kim to obtain "exact" values of the natural frequencies of [ABBCAAB]r laminate are compared with Whitney's equations. Also natural frequencies of the plate with varying aspect ratios and reinforcing fiber orientations, are compared with natural frequencies of bean. This work can be a guideline to obtain data in many other cases.

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Boundary Layer Analysis in a Hypersonic Flow Field (극초음속 유동장의 경계층 해석)

  • Sohn Chang-Hyun;Choi Seung;Moon Su-Yuon;Kim Jae-Yung;Lee Yul-Hwa
    • Journal of the Korea Institute of Military Science and Technology
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    • v.7 no.3 s.18
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    • pp.165-173
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    • 2004
  • Matching inviscid and boundary layer methods are developed for analysis of hypersonic flow with thick boundary layer. The new equations match all the boundary layer properties with a variation in the inviscid solution near the edge, except for the normal velocity. Computational comparison are peformed for incompressible and compressible flows over a flat plate. Results from the present method are compared with Wavier-Stokes solutions. The present results are in good agreement with Wavier-Stokes solutions. They show that the new technique can provide improved predictions of heating rates and skin friction predictions for preliminary design of vehicles where shear layers and entropy layer swallowing are importantfor for preliminary design.

Economic Optimization in Preliminary Ship Design (선박기본설계과정(船舶基本設計過程)에서의 경제성검토(經濟性檢討)와 최적화기법(最適化技法)의 응용(應用))

  • Z.K.,Kim;S.H.,Han
    • Bulletin of the Society of Naval Architects of Korea
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    • v.15 no.4
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    • pp.1-5
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    • 1978
  • The preliminary ship design step is made into a non-linear programming(NLP) problem. And using SUMT-exterior method and Hook Jeeves pattern search, the optimum ship characteristics are determined for the case where the ship is built in Korea and is operated by Koreans. Three programs for bulk carrier, tanker, and container ship are constructed and several sensitivity tests are performed. The result has little difference from the results of the other papers, but for high interest rate of return, slightly larger and faster ship is superior, and for low labour costs, slightly smaller and slower ship is superior.

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Preliminary Design of LEO Satellite Propulsion System (저궤도위성 추진시스템 예비 설계)

  • Yu, Myeong-Jong;Lee, Gyun-Ho;Kim, Su-Gyeom;Choe, Jun-Min
    • Aerospace Engineering and Technology
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    • v.5 no.2
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    • pp.85-89
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    • 2006
  • Propulsion System provides the required velocity change impulse for orbit transfer from parking orbit to mission orbit and three-axis vehicle attitude control impulse. New LEO Satellite propulsion system (PS) will be an all-welded, monopropellant hydrazine system. The PS consists of the subassemblies and components such as Thrusters, Propellant Tank, Pressure Transducer, Propellant Filter, Latching Isolation Valves, Fill/Drain Valves, interconnecting propellant line assembly, and thermal hardwares for operation-environment control of the PS. In this study, preliminary design process of LEO Satellite propulsion system will be summarized.

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A Case Study on the Design of Container Terminal in Vietnam

  • Choi, Yong-Seok;Kim, Woo-Sun;Choi, Sang-Hei;Ha, Tae-Young
    • Journal of Navigation and Port Research
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    • v.30 no.7
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    • pp.591-598
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    • 2006
  • Port development has been remarkably increasing due to the progress of industrialization in ASEAN area. Especially, Vietnam has increased the international physical distribution in this area rapidly. The main issues facing decision makers at container terminals in Vietnam are how to expand the existing container terminals and construct new container terminals. In this paper, we performed the basic design based on simulation analysis in order to support the expansion of Quy Nhon port in Vietnam as a case study. The preliminary capacity analysis was conducted on the one berth at the port to analyze the scale of C/C(Container Crane)and yard area. Alternative scenarios were created based on the preliminary capacity analysis and the detailed simulation analysis was conducted for supporting the scenarios.

A Study on the Economics of Container Ships at Preliminary Design Stage (초기설계단계(初期設計段階)에서의 콘테이너선(船)의 경제성(經濟性)에 관한 연구(硏究))

  • Dong-Kon,Lee;S.I.,Ma
    • Bulletin of the Society of Naval Architects of Korea
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    • v.21 no.2
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    • pp.1-7
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    • 1984
  • This paper is concerned with an optimum design study of containerships in preliminary stage by applying economic criteria. The Net Present Value Index (NPVI) and the Required Freight Rate(RFR) are used as measures of merit. Hooke & Jeeves direct search method and External Penalty Function method of Sequential Unconstrained Minimization Techniques(SUMT) are used for solving constrained nonlinear optimization problem. Sensitivity analysis is carried out to investigate the effect on the optimum solution due to change of values in some parameters such as crane capacity, load factor, oil price, ship speed and the ratio between loaded FEU and TEU.

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A Case Study on the Design of Container Terminal in Vietnam

  • Choi, Yong-Seok;Choi, Sang-Hei;Kim, Woo-Sun;Ha, Tae-Young
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 2006.10a
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    • pp.193-202
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    • 2006
  • Port development is remarkable increased due to the progress of industrialization in ASEAN area. Especially, Vietnam has increased the international physical distribution in this area rapidly. The main issues facing decision makers at container terminals in Vietnam are how to expand the existing container terminals and construct new container terminals. In this paper, we performed the basic design based on simulation analysis in order to support the expansion of Quy Nhon port in Vietnam as a case study. The preliminary capacity analysis was conducted on the one berth at the port to analyze the scale of C/C and yard area. Alternative scenarios were created based on the preliminary capacity analysis and the detailed simulation analysis was conducted fur the scenarios. And in order to establish the marketing strategy, we classified the marketing elements by industrial environment and performed SWAT analysis of the port.

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