• 한국철도학회:학술대회논문집
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• 한국철도학회 2008년도 춘계학술대회 논문집
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• pp.1227-1232
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• 2008

High-speed train of push-pull type called as G7 train has been developed and chosen as the model of KTX-II which will be operated on Honam Line nexr year. However, the EMU-type high-speed train appeared to be the recent trend that foreign markets have shown. Also, in the near future, a great number of new train sets are needed to accommodate the increased passengers in our country. Thus, development of the high-speed EMU was decided, planned, and started. In the development, included were almost all fundamental key technologies such as noise and vibration reduction in a passenger cabin, running characteristics, aerodynamic analysis, crashworthiness evaluation, EMI/EMC analysis, design of the cooling system for the propulsion control system, enhanced performance of transformer and switching converters, synchronous traction motor with permanent magnets, new design of front nose and ergonomic interiors, application of advanced information technology(IT) and smart sensors and the cost reduction of construction of railway bridges, etc. Each key technologies are carried out as sub-project independently but under the supervision of a project. The project will develop the high advanced level of technologies and provide necessary know-why's and support the team in charge of the development of the high-speed EMU, Hyundai Rotem Co. Ltd. The high-speed EMU will be successfully developed with the support of the project.

• 설비공학논문집
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• 제23권11호
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• pp.726-732
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• 2011

The aerodynamic and aeroacoustic performance of discharge grille of outdoor unit of air-conditioner was investigated in this study. Discharge grille is one of outdoor unit's important parts to affect the flow rate and Overall Sound Pressure Level(OSPL). New type of discharge grille was suggested based on the results of numerical simulation. To simulate the flow pattern near the propeller fan, commercial flow solver FLUENT was used. Sliding mesh method was used for rotating propeller fan and initial condition for unsteady model was calculated by Multiple Reference Frame(MRF) method. To minimize the interaction noise between fan blade wake and discharge grille, new discharge grille has radial rib which is aligned with trailing edge of fan blade. And inclined radial rib was adopted for reducing flow rate drop in discharge grille. The optimization of inclined angle of radial grille was performed experimentally.

• 항공우주기술
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• 제5권2호
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• pp.102-107
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• 2006

본 논문은 위성체 동적 환경의 발사체 구조에 의해 전달된 저 주파수의 과도 진동과 불 규칙적인 가속력으로 구성되어 있다. 저 주파수에서의 과도 진동은 보통 진동수 100 ~ 200Hz에 이르는 정현파로 근사되며 주로 예비설계에 사용된다. 그리고, 랜덤 환경은 발사체의 연소와 분리 단계, 외부 공력소 음에 의한 구조적 진동에 의해 발생한다. 이는 발사체 구조물을 통하여 위성체와 발사체의 어댑터 구조로 전달된다. 이러한 동적환경 중에서 랜덤 진동 해석은 위성체에 수행되는데, 특히, 위성체 내의 전자 박스(장비) 는 실제 상황에 가깝게 하여 검증하기 위해 랜덤 진동 실험을 통해 설계 되야 한다.

• 대한기계학회논문집A
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• 제21권6호
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• pp.942-950
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• 1997

Far field acoustic pressure from the evolution and interaction of three-dimensional vortex filament is calculated numerically. A vortex ring is a typical example of the three-dimensional vortex filament. An elliptic vortex ring emits a strong sound signal due to significant distortion and stretching of the vortec filament. The far field acoustic pressure is linearly dependent on the third time derivatives of the vortex positions. A numerical scheme of high resolution is employed to describe in detail the elliptic vortex ring motions which ar highly nonlinear. Descretized vortex filaments are interpolated by using a parametric blending function to remove a possible numerical instability. The distorted vortex filament, owing to the self-induced and the induced velocity from the other vortex segments, is redistributed at each time step. The accuracy and efficiency of the scheme are validated by comparisons with the analytic solution of circular vortex ring interaction.

• 한국항공우주학회지
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• 제31권7호
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• pp.69-74
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• 2003

Vane tip 개념을 도입하여 소음 특성을 개선하도록 설계된 차세대 로터 블레이드(NRSB-I)의 공력 성능을 기존의 BERP 블레이드와 비교하기 위하여, 제자리 비행에 대한 점성 압축성 계산을 수행하였다. 깃끝 영역의 면적감소에 의하여 설계된 로터 블레이드의 절대 추력이 6-7% 정도 감소하지만, 동력계수의 감소폭이 더 크기 때문에 제자리 비행 성능상의 손실은 거의 없는 것으로 파악되었다. 또한, 깃끝 절단부에서 발생한 와류는 블레이드 표면을 지날 때 확산에 의하여 그 강도가 현저하게 약화되므로, 설계요구조건을 만족시키기 위해서는 절단부 위치에 펜스가 필요함을 확인할 수 있었다.

• 한국항공우주학회지
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• 제46권2호
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• pp.159-166
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• 2018

본 연구에서는 소형민수헬기(Light Civil Helicopter, LCH)의 풍동시험에 필요한 축소 로터 블레이드에 대해 내부 구조설계와 동특성 및 하중해석을 수행하였다. 축소로터 풍동시험은 로터 시스템의 공력성능과 소음 특성을 평가하기 위해 수행되므로, 실제 크기의 로터시스템과 동일한 공력 특성을 모사할 수 있도록 축소 블레이드 설계 시 마하 스케일(Mach-scale) 기법을 적용하였다. 마하 스케일 블레이드는 실물 블레이드의 끝단속도(blade tip speed)와 동일한 값을 유지할 수 있도록 로터의 회전속도를 증가시켜야 하며, 블레이드 중량, 단면강성 및 고유진동수 등은 특정한 축소계수(${\lambda}$, scaling factor)를 통해 조정된다. 블레이드 내부의 주요 구성품인 스킨, 스파, 토션박스 등을 설계하기 위해 탄소섬유와 유리섬유 계열의 복합소재를 적용하였으며, 국내에서 수급이 가능한 프리프레그(prepreg) 형태의 복합소재를 적용하였다. 내부구조 설계가 완료된 블레이드에 대해 단면강성을 평가하기 위해 KSec2D 프로그램을 사용하였으며, 회전익 항공기의 통합해석 프로그램인 CAMRADII를 이용하여 축소 블레이드의 하중 분포와 동역학적 특성을 검토하였다.

• Journal of Astronomy and Space Sciences
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• 제26권1호
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• pp.31-46
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• 2009

An Unscented Kalman Filter (UKF) for estimation of the attitude and rate of a spacecraft using only magnetometer vector measurement is developed. The attitude dynamics used in the estimation is the nonlinear Euler's rotational equation which is augmented with the quaternion kinematics to construct a process model. The filter is designed for small satellite in low Earth orbit, so the disturbance torques include gravity-gradient torque, magnetic disturbance torque, and aerodynamic drag torque. The magnetometer measurements are simulated based on time-varying position of the spacecraft. The filter has been tested not only in the standby mode but also in the detumbling mode. Two types of actuators have been modeled and applied in the simulation. The PD controller is used for the two types of actuators (reaction wheels and thrusters) to detumble the spacecraft. The estimation error converged to within 5 deg for attitude and 0.1 deg/s for rate respectively when the two types of actuators were used. A joint state parameter estimation has been tested and the effect of the process noise covariance on the parameter estimation has been indicated. Also, Monte-Carlo simulations have been performed to test the capability of the filter to converge with the initial conditions sampled from a uniform distribution. Finally, the UKF performance has been compared to that of the EKF and it demonstrates that UKF slightly outperforms EKF. The developed algorithm can be applied to any type of small satellites that are actuated by magnetic torquers, reaction wheels or thrusters with a capability of magnetometer vector measurements for attitude and rate estimation.

• 대한후두음성언어의학회지
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• 제18권1호
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• pp.44-50
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• 2007

Background and Objectives: The 585-nm pulsed dye laser (PDL) has recently been adopted by otolaryngologists because of its epithelial-sparing properties. Many authors have reported the use of PDL for treatment of various vocal cord lesions. This purpose of this study is to examine the effectiveness of 585-nm PDL in the treatment of vocal polyp. Materials and Methods: Eight patients with vocal polyp were treated with 585-nm PDL from Sep. 2006 to Nov. 2006 in Yong-dong Sevrance hospital. 5 of them went through local anesthesia and 3 of them went through general anesthesia. In order to control laser fiber, flexible digital transnasal laryngoscope was applied under local anesthesia and general anesthesia using LMA, and micromanipulator was used under general anesthesia using endotracheal tube. The evaluations of vocal function was done at pre-and postoperation. Results: All patients improved in the perceptual evaluation of voice after PDL surgery. The aerodynamic study revealed that 5 of 8 patients showed improvement in maximal phonation time, and 6 of 8 showed improvement in mean airflow rate during phonation. The acoustic analysis revealed that all patients showed improvement in Jitter and Shimmer, and 7 of 8 showed improvement in noise to harmony ratio. Conclusion: This study demonstrates promising results in the efficacy of 585-nm PDL for the treatment of vocal polyps, and it illustrates a new option for vocal polyp treatment as well as the advantage of PDL surgery.

• 대한후두음성언어의학회지
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• 제29권2호
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• pp.83-86
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• 2018

Background and Objectives : This study aimed to evaluate efficacy and complication of injection laryngoplasty using calcium hydroxyapatite (CaHA) for unilateral vocal fold paralysis in Asian. Materials and Methods : A prospective study was conducted on the adult patients with unilateral vocal fold paralysis from May 2015 through January 2016. Injection laryngoplasty was performed by one laryngologist. All patients underwent prospective voice evaluation using the subjective and objective comprehensive battery of assessments, before the procedure and after the procedure at 3 months, and 6 months. Results : A total of 7 patients (5 males and 2 females) were included in this study. VHI-10 was significantly decreased after injection laryngoplasty, at postoperative 6 months (p=0.031), while VAS score and MDADI showed no difference. GRBAS scale gradually decreased in 3 months and 6 months follow-up without statistical significance. Acoustic analysis revealed that jitter, shimmer, and noise-to-harmonic ratio continuously decreased from the baseline at 3 months and 6 months, although statistical significance was not attained. In the aerodynamic analysis, maximal phonation time was gradually increased at 3months and 6 months with significant difference (p=0.016, 0.031, respectively). There was no side effect associated with the procedure. Conclusion : CaHA can be safely used in Asian patients and the onset of maximal efficacy seems to be slow than other studies with Caucasian patients.

• 한국군사과학기술학회지
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• 제26권1호
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• pp.1-9
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• 2023

The skin structure of sensor pod mounted on the exterior of aircraft can be exposed to the acoustic dynamic load and static load such as aerodynamic pressure and inertial load during flight. Fatigue life prediction of structural model under acoustic load should be performed and also differential stiffness of model modified by static load should be considered. The acoustic noise test spectrum of MIL-STD-810G was applied to the structural model and the stress response power spectral density (PSD) was calculated. The frequency response analysis was performed with or without prestress induced by inplane static load, and the response spectrum was compared. Time series data was generated using the calculated PSD, and the time and frequency domain fatigue life were predicted and compared. The variation of stress response spectrum due to static load and predicted fatigue life according to the different structural model considering mean stress were examined and decreasing fatigue life was observed in the model with prestress of compressive static load.