• 제목/요약/키워드: Design space exploration

검색결과 195건 처리시간 0.025초

Design Study on a Variable Intake and a Variable Nozzle for Hypersonic Engines

  • Taguchi, Hideyuki;Futamura, Hisao;Shimodaira, Kazuo;Morimoto, Tetsuya;Kojima, Takayuki;Okai, Keiichi
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.713-721
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    • 2004
  • Variable air intake and variable exhaust nozzle of hypersonic engines are designed and tested in this study. Dimensions for variable geometry air intake, ram combustor and variable geometry exhaust nozzle are defined based on the requirements of a pre-cooled turbojet engine. Hypersonic Ramjet Engine is designed as a scaled test bed for each component. Actuation forces of moving parts for variable intake and variable nozzle are reduced by balancing the other force in the opposite direction. A demonstrator engine which includes variable intake and variable nozzle is designed and the components are fabricated. Composite material with silicone carbide is applied for high temperature parts under oxidation environment such as leading edge of the variable intake and combustor liner. Internal cooling structure is adopted for both moving and static parts of the variable nozzle. Pressure recovery and mass capture ratio of the variable intake at Mach 5 is obtained by a hypersonic wind tunnel test. Flow characteristics of the variable nozzle are obtained by a low temperature flow test. Wall temperature and heat flux of the nozzle at Mach 3 is obtained by a firing test. As results, the intake and the nozzle are proved to be used at designed pressure and temperature environment.

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Experimental Study of the Multi-Row Disk Inlet

  • Maru, Yusuke;Kobayashi, Hiroaki;Kojima, Takoyuki;Sato, Tetsuya;Tanatsugu, Nobuhiro
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.634-643
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    • 2004
  • In this paper are presented a concept of a new supersonic air inlet, which is designated a Multi-Row Disk (MRD) inlet, aiming at performance improvement under off-design conditions, and results of wind tunnel tests examined performance characteristics of the MRD inlet. The MRD inlet is frequently called ‘a skeleton inlet’ because of its appearance. The performance of a conventional axisymmetric inlet with a solid center body (spike) deteriorates under off-design Mach number conditions. It is due to the fact that total pressure recovery (TPR) governed by the throat area of inlet and mass capture ratio (MCR) governed by an incidence position of an oblique shock from the spike tip into the cowl can not be controlled independently in such air inlet. The MRD inlet has the spike that is composed of a tip cone and several disks arranged downstream of it, based on the experimental fact that several deep cavities on a conical surface have little negative effect on the boundary layer growth. The overall spike length of the MRD inlet is adjustable to the given flight speed by changing space between disks so that a spillage flow can be controlled independently from controlling the throat area. It could be made clear from the result of wind tunnel tests that the MRD inlet improves TPR by 10% compared with a conventional inlet with a solid spike under off-design conditions.

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카페공간에 대한 수렴적 탐색상황에서의 주의집중 특성의 분석 방법에 관한 연구 - 선택적 주시데이터에 의한 뇌파 데이터 분석을 중심으로 - (A Study on the Attention Concentration Properties in Convergent Exploration Situations in Cafe Space - Focusing on Gaze and Brain wave Data Analysis -)

  • 김종하;김주연;김상희
    • 한국실내디자인학회논문집
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    • 제25권2호
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    • pp.30-40
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    • 2016
  • This study analyzed the attention concentration tendencies of one(1) subject who showed convergent exploratory acts actively through the gaze-brainwave measurement experiment of cafe space images and our research findings are as follows. First, the areas of interest (AOIs) that the subject gazed visually by paying attention to it and concentrating on it at a cafe space include counter&menu area, sign area, partition area, image wall area, stairs area, and movable furniture area, and built-in furniture area: seven areas in total. Second, conscious gaze frequency appeared the highest in counter&menu area, and conscious gaze appeared more later than in initial times. Third, conscious gaze pattern was divided into the zone that explored various areas dispersely (distributed exploratory zone) and the zone that explored between particular areas concentratedly (intensive exploratory zone). Fourth, as a result of analyzing the brainwave attention concentration, it was found that the attention concentration in prefrontal lobe (Fp1, Fp2) and frontal lobe (F3, F4) rose to a higher level in the zone of 15 to 16 seconds and this time zone was considered to be a zone where gazing at counter&menu area was very active. In addition, the attention concentration appeared higher in the initial zone than in the later zone, among the entire experimental time zones. Finally, as a result of analyzing the changes in activation by brain portion of the SMR wave expressed when maintaining the arousal and attention concentration, it was found that the right prefrontal lobe and the frontal lobe became activated in the time zone when the intensive exploration of "counter&menu area" and "movable furniture${\leftrightarrow}$built-in furniture area" had occurred and the time zone when the intensive exploration of "image wall${\leftrightarrow}$partition area" and "counter&menu${\leftrightarrow}$sign area" had occurred.

소형위성 전용 발사체를 이용한 심우주 임무 설계 (Design of Deep Space Missions Using a Dedicated Small Launch Vehicle)

  • 최수진;;;서대반;이기주
    • 한국항공우주학회지
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    • 제50권12호
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    • pp.877-888
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    • 2022
  • 최근 루나 게이트웨이의 선구자 임무인 CAPSTONE이 NRHO에서 통신 및 항법 기술 시연을 위해 소형발사체로 발사됨에 따라 전용 소형발사체와 소형위성을 이용하여 심우주 임무를 가능하게 한 이번 행사가 큰 주목을 받았다. 본 연구에서는 소형발사체 이중발사 운영개념이 소개하고, 달, 화성 및 소행성 탐사를 위한 새로운 개념의 가능성을 검토했다. 단독발사로 달 저궤도 임무에 약 247 kg을, 이중발사로 화성 및 소행성 아포피스와 같은 목적지에 각각 215 kg 및 183 kg을 수송할 수 있는 것으로 나타났다.

우주생명현상과 성간천체 탐사 전망 (THE PROSPECT OF INTERSTELLAR OBJECT EXPLORATIONS FOR SEARCHING LIFE IN COSMOS)

  • Minsun Kim;Ryun Young Kwon;Thiem Hoang;Sungwook E. Hong
    • 천문학논총
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    • 제38권2호
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    • pp.25-36
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    • 2023
  • Since interstellar objects like 1I/'Oumuamua and 2I/Borisov originate from exoplanetary systems, even if we do not visit the exoplanetary systems, flyby, rendezvous, and sample return missions of interstellar objects can provide clues to solve the mysteries of cosmic life phenomena such as the origin of exoplanetary systems, galactic evolution, biosignatures (or even technosignatures), and panspermia. In this paper, we review space missions for interstellar object exploration in the stage of mission design or concept study such as Project Lyra, Bridge, Comet Interceptors, and LightcraftTM. We also review space missions, OSIRIS-REx and NEA Scout, designed for Near Earth Asteroids(NEA) explorations, to investigate the current state of basic technologies that can be extended to explore interstellar objects in a velocity of ~ 6AU/year. One of the technologies that needs to be developed for interstellar object exploration is a spacecraft propulsion method such as solar sail, which can catch up with the fast speed of interstellar objects. If this kind of propulsion becomes practical for space explorations, interstellar object explorations will mark a new era and serve as a driving force to provide evidences of cosmic life.

인공지능 응용을 위한 하이브리드 메모리 설계 탐색 기법 (An Design Exploration Technique of a Hybrid Memory for Artificial Intelligence Applications)

  • 조두산
    • 한국산업융합학회 논문집
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    • 제24권5호
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    • pp.531-536
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    • 2021
  • As artificial intelligence technology advances, it is being applied to various application fields. Artificial intelligence is performing well in the field of image recognition and classification. Chip design specialized in this field is also actively being studied. Artificial intelligence-specific chips are designed to provide optimal performance for the applications. At the design task, memory component optimization is becoming an important issue. In this study, the optimal algorithm for the memory size exploration is presented, and the optimal memory size is becoming as a important factor in providing a proper design that meets the requirements of performance, cost, and power consumption.

Tapping the Potential of Roof Greening and Building a New City-scape

  • Wang, Xiao-yun
    • Journal of the Korean Institute of Landscape Architecture International Edition
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    • 제1호
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    • pp.33-36
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    • 2001
  • Only do we have an earth! It is crucially important to improve our living environment and keep the sustained development of a city in the limited space. Some concrete examples will be analysized in the paper, elaborating upon how to make full use of roof space and various plants to create a better green-space. To create different activity space with unique characteristics for people, various plants, roof-space, water and buildings in the style of garden should be use when local conditions and design requirement should be considered.

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슈퍼스칼라 프로세서 시뮬레이터의 생성을 위한 Attributed AND-OR 그래프 (Attributed AND-OR Graph for Synthesis of Superscalar Processor Simulator)

  • Jun Kyoung Kim;Tag Gon Kim
    • 한국시뮬레이션학회:학술대회논문집
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    • 한국시뮬레이션학회 2003년도 춘계학술대회논문집
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    • pp.73-78
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    • 2003
  • This paper proposes the simulator synthesis scheme which is based on the exploration of the total design space in attributed AND-OR graph. Attributed AND-OR graph is a systematic design space representation formalism which enables to represent all the design space by decomposition rule and specialization rule. In addition, attributes attached to the design entity provides flexible modeling. Based on this design space representation scheme, a pruning algorithm which can transform the total design space into sub-design space that satisfies the user requirements is given. We have shown the effectiveness of our framework by (ⅰ) constructing the design space of superscalar processor in attributed AND-OR graph (ⅱ) pruning it to obtain the ARM9 processor architecture. (ⅲ) modeling the components of the architecture and (ⅳ) simulating the ARM9 model.

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우주 행성 탐사 로버 등판 시험장 설계 (Space Planet Exploration Rover Climbing Test Site Design)

  • 유병현
    • 한국지반신소재학회논문집
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    • 제22권4호
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    • pp.1-8
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    • 2023
  • 우주 탐사는 인류의 과학적 노력 중 가장 선두에 있으며, 행성 탐사 로버는 행성 지표면을 연구하는 핵심 장비이다. 행성 로버의 성능은 가파른 경사와 다양한 행성 지형을 탐지하고 통과하는 데 큰 영향을 미치며 특히 달과 같은 행성에서는 급격한 경사와 연약한 지면을 안전하게 등반하고 이동할 수 있는 능력이 필수적으로 요구된다. 이 논문에서는 우주 행성 탐사 로버가 직면하는 가파른 지형과 연약한 지면을 모사하는 등반 시험장의 설계와 검증 방법을 종합적으로 소개한다. 먼저 달의 크레이터 지역의 지형 특성과 탐사의 중요성을 간략히 설명하고, 기존 등반 시험장의 개발 사례를 살펴보며, 현재 한국건설기술연구원에서 운영 중인 지반열진공챔버 내에 설치 예정인 등반 시험장의 설계 과정을 설명한다. 본 연구에서 제안하는 등반 시험장이 개발되면 실제 달의 환경과 유사한 고진공, 극한 온도 조건에서 로버의 이동과 탐사 능력을 정밀하게 평가할 수 있을 것으로 기대된다.