• Title/Summary/Keyword: CRW

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CFD Analysis of External Balance Strut Supporting Wind Tunnel Model (CFD를 이용한 풍동 시험 모델 지지대의 공력 특성 해석)

  • Kim C. W.;Park Y. M.;Lee J. Y.
    • 한국전산유체공학회:학술대회논문집
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    • 2003.08a
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    • pp.102-105
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    • 2003
  • The effect of the external balance strut on the wind tunnel model is investigated with simplified geometries. For this study, flat plate and elliptic wing are simulated with and without a cylinder. Pressure and wall shear stress distribution are analyzed to understand the effect of the cylinder.

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Dynamic Aeroelastic Characteristics of an All-Movable Canard with Oscillating Flap Used in UAV (플랩이 있는 무인기 전운동 카나드의 동적공탄성 특성)

  • Kim, Dong-Hyun;Koo, Kyo-Nam;Lee, In;Kim, Sung-Jun;Kim, Sung-Chan;Lee, Jung-Jin;Choi, Ik-Hyun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.6
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    • pp.56-63
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    • 2004
  • In this study, dynamic aeroelastic analyses of the canard with oscillating flap are conducted considering the effect of aerodynamic compressibility. The canard model considered herein is an all-movable type with a pitching axis on a canard-rotor-wing aircraft which was considered as one of the major UAV candidates under developing in Korea. The equivalent structural model is constructed based on the initial design data by the Korea smart UAV development center. Both the frequency and the time-domain aeroelastic analyses have been applied to practically conduct parametric studies on the effects of equivalent torsional stiffness. In the case of all-movable control surface with oscillating flap, the equivalent rotational stiffness of the pitch axes are important design parameters. The parametric results for the aeroelastic instability are practically presented.

Development of Image Guided 3D Localization Program for Stereotactic Brain Biopsy (뇌 정위 생검술을 위한 영상지원 3차원 국재 프로그램 개발)

  • Lee Do Heui;Lee Dong Joon
    • Progress in Medical Physics
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    • v.15 no.4
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    • pp.197-201
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    • 2004
  • Stereotactic brain biopsy using stereotactic head frame such as CRW (Radionics, USA) has demonstrated a precise lesion localizing accuracy. In this study, we developed the target point calculation program for brain lesion biopsy using CRW stereotactic head frame and designed a phantom for verify the new developed program. The phantom was designed to have capability to simulate clinical stereotactic brain biopsy. The phantom has 10 vertical rods whose diameters are 6mm and tip of each rods are 2mm. Each rod has different length, 150 mm x 4 ea, 130 mm x 4 ea, 110 mm x 2 ea. CT images were acquired with Simens CT scanner as continuous transverse slice, 1 mm thickness in a 25 cm field of view and stored in a dicom file as a 256 x 256 matrix. As a result, the developed new target localization program will be useful for planning and training in complicated 3 dimensional stereotactic brain biopsy.

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Steady State Operational Characteristic Analysis of the Propulsion System for the Canard Rotor Wing UAV in three different Flight Modes (비행 모드에 따른 CRW UAV 추진시스템의 정상상태 운전특성 해석)

  • 공창덕;강명철;기자영;박종하;양수석;전용민
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2003.10a
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    • pp.215-218
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    • 2003
  • In this study, a performance model of the Smart UAV propulsion system with ducts, tip jets and variable main nozzle, which has flight capability of the rotary wing mode for the take-off/landing and low speed forward flight as well as the fixed wing mode for high speed forward flight, has been newly developed. With the proposed model, steady-state performance analysis was performed at various flight modes and conditions, such as rotary wing mode, fixed wing mode, compound wing, mode altitude and flight speed.

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Canard Rotor/Wing 비행체 추진시스템의 회전익 및 천이모드 성능

  • Lee, Chang-Ho
    • Aerospace Engineering and Technology
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    • v.3 no.2
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    • pp.50-55
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    • 2004
  • Performance predictions of the propulsion system were conducted for a 900㎏ class Canard Rotor/Wing vehicle. The main components of the propulsion system are turbojet engine, exhaust ducts and nozzles. The internal flow of the duct was considered as one-dimensional, compressible and viscous flow. Adequate governing equations including centrifugal force effect were applied to the analysis of the duct flows. Results such as available power, available thrust, engine throttle, mass flow rates, rotor RPM and cruise nozzle area were presented for rotary-wing mode and transition mode.

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An Analysis on RAW Image File of DLSR Camera and Development of a RAW Image Viewer for an Embedded Device (DLSR 카메라의 RAW 이미지 파일 분석 및 임베디드 장치용 RAW 이미지 뷰어 개발)

  • Ro, Kwang-Hyun;Kim, Seung-Cheon
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.12 no.3
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    • pp.1341-1349
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    • 2011
  • This research is focused on an analysis on the structure of RAW image file and the development of a RAW image file viewer for an embedded device. Recently, several RAW image file formats are being used for saving and displaying the images created by various DSLR cameras, and the necessity of handing RAW images in mobile multimedia devices is increasing. For the development of RAW image decoding/encoding library applicable to WinCE-based embedded devices viewer, an analysis of RAW image file formats, such as CRW, CR2, PEF, NEF, MRW, have been performed because their formats are not released in public. By using the library, the analysis software which can extract RAW image data, 2~3 JPEG image files and other informations such as the specification of a camera and various photographic parameters from RAW image files, were developped and a RAW image file viewer which can run in WinCE-based embedded devices. The experimental result has shown that the viewer could encode and decode RAW image files successfully and it took approximately 10secs to load them to the screen in S3C6410 based embedded platform. The outcomes of this research cloud be a good information and solution to multimedia application developers.

Conceptual Study and Design Ideas for SUAV Propulsion System (스마트무인기 신개념추진시스템 개념연구)

  • 전용민;정용운;양수석
    • Journal of the Korean Society of Propulsion Engineers
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    • v.7 no.4
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    • pp.19-26
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    • 2003
  • In this paper, the result of the conceptual study of a tipjet driven propulsion system is presented. The concept of a tipjet driven propulsion system is to employ tipjet as power source to drive a rotor Because the vehicle is supposed to takeoff and land vertically, a rotor system, which has tipjet nozzles, is adopted to fly like a helicopter. Exhaust gas, which is generated by an engine, Passes through an internal duct system and divided into four blade ducts. The design code is consists of two parts, engine model and internal duct model. Inside a rotating duct, compressible flow is affected by two additional force terms, centrifugal force and coriolis force and they govern the performance in rotary mode, The intention of this paper is to address the issues associated with sizing and optimizing configurations of a tipjet driven propulsion system especially in rotary wing mode.

An Analysis on RAW Image Format and its Application for Portable Multimedia Devices (휴대용 멀티미디어기기를 위한 RAW 이미지 포맷 분석 및 응용)

  • Park, Mi-Ran;Sin, So-Hee;Kim, Jae-Shin;Ro, Kwang-Hyun
    • Proceedings of the KAIS Fall Conference
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    • 2009.05a
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    • pp.738-741
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    • 2009
  • 본 논문에서는 RAW 이미지 포맷 중 PEF, MRW에 대한 분석 결과와 RAWImage Viewer에 대해 소개한다. DSLR 디지털 카메라로 촬영되는 이미지 파일은 범용의 JPEG 포맷이나 제조사별 독자적인 RAW 이미지 포맷으로 저장된다. 이러한 RAW 이미지 파일을 PMP 등의 휴대용 멀티미디어 기기나 디지털액자에서 재생 및 확인하기 위한 요구가 증대되고 있다. 하지만, RAW 이미지 포맷이 디지털 카메라 제조사별로 다르고, 해당 포맷에 대한 구체적인 정보가 공개되지 않아 대부분의 휴대용 멀티미디어 기기에서 RAW 이미지 파일 재생 기능을 완벽하게 지원하지 못하고 있다. 본 논문에서는 RAW 이미지 파일 포맷을 분석하여 다양한 임베디드 멀티미디어 기기에서 모든 RAW 이미지 파일을 지원할 수 있는 라이브러리 구축을 위한 연구 결과 중 일부를 소개한다. Cannon의 CRW, CR2 포맷과 Nikon의 NEF 분석 결과에 이어 PEF, MRW에 대한 분석 결과와 RAW 이미지 출력 및 분석 기능이 포함된 RAWImage Viewer에 대해 설명한다. 연구 결과는 RAW 파일을 재생할 수 있는 임베디드 장비 및 PC용 RAW 이미지 파일 재생 라이브러리를 구축 및 응용 프로그램 개발시 활용될 것이다.

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The Development of Performance Analysis Code for Pre-Conceptual Design of VTOL UAV (수직이착륙/고속순항 무인기 초기개념설계를 위한 성능예측 프로그램 개발)

  • Jung, Won-Hyung;Lee, Kyung-Tae;Kim, Jung-Yub
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.5
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    • pp.1-9
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    • 2004
  • The performance analysis code has been developed for vertical take-off and landing(VTOL) UAV which can be utilized as a trade analysis tool in the pre-conceptual design phase. The UAV requires VTOL capability and high speed cruise performance. The main logic of this performance analysis code is to estimate performance parameters of each mission segment by mission fuel weight iteration. The reliability of this performance analysis code is discussed by comparing the data of existing dual flight mode VTOL UAVs such as Boeing CRW and Bell Tilt Rotor.

Clinical Analysis of Stereotactic Biopsy in Brain Lesions (정위적 뇌생검의 임상분석)

  • Kim, Young Wook;Kim, Jae Hyoo;Seo, Seung Kweon;Lee, Jung Kil;Kim, Tae Sun;Jung, Shin;Kim, Soo Han;Kang, Sam Suk;Lee, Je Hyuk
    • Journal of Korean Neurosurgical Society
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    • v.29 no.1
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    • pp.15-22
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    • 2000
  • Objective : This study was undertaken to evaluate the benefits and risks of the stereotactic biopsy in brain lesions. We assessed the diagnostic accuracy and morbidity rate associated with the stereotactic biopsy. Methods : The authors present a review of 47 patients, who underwent stereotactic biopsy using Cosman-Roberts-Wells(CRW) stereotactic apparatus during last six years. Results : Target locations were supratentorial in 36 cases, infratentorial in 9 and multiple in 2. According to pathological diagnosis, the largest group was neoplasm(29) followed by infection(9), infarction(2), cyst(2), and non-specific(5). Definitive diagnosis could be made in 42 of 47 cases(89.4%). When the mass lesion had been suspected as neoplastic condition, the diagnostic rate was 96.7%(29/30). It was being much higher than that of non-neoplastic lesion, 76.5%(13/17). The treatment modality was changed in 15 cases(32%) because the result of stereotactic biopsy was different from clinical diagnosis. Subsequent craniotomy after stereotactic biopsy was then performed in 6 cases, and the pathological diagnoses were precisely coincident in all of these cases. There were two complications(4.3%) : One intratumoral hemorrhage in glioblastoma and a transient hemiparesis in benign astrocytoma. There was no mortality in this series. Conclusion : The precise histological verification is crucial to determine the adequate treatment modality in intracranial lesions. Stereotactic biopsy is a safe and accurate diagnostic procedure for intracranial lesions with a low complication rate.

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