• 항공우주기술
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• 제11권2호
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• pp.208-215
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• 2012

우주발사체 비행에 의한 발사장 주변의 음향 소음에 대하여 분석하였다. 발사체 엔진 배기 제트에 소음원을 위치시키고 소음의 방향성, 대기 감쇄 등을 고려하여 발사장 주변의 특정 지점에 미치는 소음의 크기를 예측하였다. KSLV-I의 발사 소음을 예측하고 이 결과를 비행시험시의 측정 결과와 비교하였다. 분석 결과는 소음의 방향성에 의해 큰 영향을 받는 것으로 나타났으며 소음 방향성 정보에 대한 적절한 가정에 의해 시험 결과와 예측 결과가 서로 잘 일치하는 것을 확인하였다.

• 한국항공우주학회지
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• 제35권9호
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• pp.826-835
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• 2007

발사체 열환경 설계를 위해서 여러 종류의 태양열 모델을 비교 검토하였으며, 측정된 태양열과 잘 일치하는 태양열 모델을 개발하였다. 기존의 태양열 모델은 태양 직사광 예측은 정확하지만 산란광에 대해서는 오차가 포함되어 있었다. 이에 반하여 새롭게 개발된 산란광 모델은 등방성, 이방성 산란을 고려하였으며 기존의 어느 모델보다 관측값과 잘 일치하였다. 우주 센터의 태양광 측정 데이터가 매우 적기 때문에 본 모델은 발사체 열하중 설계에 필요한 설계 데이터를 제공할 수 있었다. 또한 본 모델은 위도, 경도, 날짜, 고도에 대한 제한이 없는 일반적인 모델이기 때문에 추후 태양열에 민감한 반응을 보이는 비행기구 등의 개발에 효과적인 열환경 예측 수단을 제공할 수 있다.

• 한국추진공학회지
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• 제24권2호
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• pp.73-82
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• 2020

저비용 발사체를 개발 중인 많은 스타트업들이 소형 로켓 엔진을 확보하기 위해 적층제조 기법을 개발 중이다. 또한, 미국의 SpaceX, Rocket Lab 등을 비롯하여, 유럽의 Ariane Group, 일본의 IHI와 같은 엔진 제작업체들은 로켓 엔진의 주요부품에 적층제조를 채택하여 생산하고 있다. 본 논문에서는 적층제작기법의 타당성을 조사하기 위해서 기존 로켓 엔진의 밸브 하우징을 적층제조 하는 사례연구 결과를 소개한다.

• 한국소음진동공학회논문집
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• 제17권12호
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• pp.1208-1216
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• 2007

Turbomachinery such as turbines, pumps and compressors, which are installed in transportation systems, including aircrafts, ships, and space vehicles, etc., often perform crucial missions and are exposed to potential dangerous impact environments such as base-transferred shock forces. To protect turbomachinery from excessive shock forces, it may be needed to accurately analyze transient responses of their rotors, considering the dynamics of mount designs to be applied. In this study a generalized FE transient response analysis model, introducing relative displacements, is proposed to accurately predict transient responses of a flexible rotor-bearing system with mount systems to base-transferred shock forces. In the transient analyses the state-space Newmark method of a direct time integration scheme is utilized, which is based on the average velocity concept. Results show that for the identical mount systems considered, the proposed FE-based detailed flexible rotor model yields more reduced transient vibration responses to the same shocks than a conventional simple model, obtained by treating a rotor as concentrated lumped mass, equivalent spring and a damper or Jeffcott rotor model. Hence, in order to design a rotor-bearing system with a more compact light-weighted mount system, preparing against any potential excessive shock, the proposed FE transient response analysis model herein is recommended.

• International Journal of Aeronautical and Space Sciences
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• 제2권2호
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• pp.1-18
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• 2001

A numerical technique for simulating the separation dynamics of strap-on boosters jettisoned in the dense atmosphere is presented. Six degree of freedom rigid body equations of motion are integrated into the three-dimensional unsteady Navier-Stokes solution procedure to determine the dynamic motions of strap-ons. An automated Chimera overlaid grid technique is introduced to achieve maximum efficiency for multi-body dynamic motion and a domain division technique is implemented in order to reduce the computational cost required to find interpolation points in the Chimera grids. The flow solver is validated by comparing the computed results around the Titan IV launch vehicle with experimental data. The complete analysis process is then applied to the. H-II launch vehicle, the central rocket in japans space program, the CZ-3C launch vehicle developed in China and the KSR-III, a three-stage sounding rocket being developed in Korea. From the analyses, separation trajectories of strap-on boosters are predicted and aerodynamic characteristics around the vehicles at every time interval are examined. In addition, separation-impulse devices generally introduced for safe separation of strap-ons are properly modeled in the present paper and the jettisoning force requirements are examined quantitatively.

• 한국항공우주학회지
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• 제43권1호
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• pp.88-95
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• 2015

본 논문에서는 액체 엔진의 혼합비 오차와 추진제 탑재 오차가 성능에 미치는 영향에 대해서 분석하였다. 75톤급 엔진 4개를 클러스터링하는 발사체 모델에 대해 이런 오차에 의해 발생하는 추진제 잔류량을 확률적인 Monte-Carlo 방법을 사용하여 계산하고 잔류량을 최소화할 수 있는 최적 연료 바이어스를 도출하였다. 다른 발사체에 사용된 근사식을 사용한 해석적인 방법과 비교함으로써 얻어진 결과의 타당성을 검토하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제36회 춘계학술대회논문집
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• pp.175-178
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• 2011

본 논문에서는 자세제어용 추력기에 사용되는 단일액체추진제의 성능특성 및 활용현황을 조사한다. 과산화수소는 단일추진제로서 1960년대 중반까지 활발히 사용되었으나, 비추력 성능과 저장성이 탁월한 하이드라진으로 급속히 대체되었다. 하이드라진은 양호한 성능특성을 배경으로 인공위성, 행성간 탐사선, 우주발사체 등의 단일추진제로서 가장 많이 사용되고 있다.

• Proceedings of the National Institute of Ecology of the Republic of Korea
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• 제2권4호
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• pp.274-278
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• 2021

Road structures play an important role in collisions involving vehicles and wildlife. Our study aimed to determine the effect of various types of road structures on the risk associated with roadkill. We surveyed 50 previously identified roadkill hotspots, ranked from one to five according to roadkill density. We collected nine types of road structure data on each hotspot road section. Structures with similar characteristics were grouped together, resulting in five categories, namely, median barrier, high edge barrier, low edge barrier, speed, and visibility. We examined the existence of each road structure category at each hotspot rank. The cumulative link model showed that the absence of bottom blocked median barrier increased the roadkill hotspot rank. Our study concluded that a visual obstacle in the middle of roads by the median barrier decreases wildlife road crossing attempts and roadkill risk. We suggest that future roadkill mitigation plans should be established considering these characteristics.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2009년도 추계학술대회 논문집
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• pp.130-136
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• 2009

The goal of this paper is to develop a standard side mirror geometry that will perform well across multiple vehicles. One of the important performance attributes of a side mirror is the amount of wind noise generated under the flow conditions on a car. PowerFLOW can be used for Computer Aided Testing of the aeroacoustics performance of a design in addition to directing design modifications based on a detailed analysis of the flow structures responsible for the noise generation. Alternatively, a Design of Experiment (DOE) approach is useful to explore the design space without any a-priori assumptions of the effects of design parameter changes. Some general design guidelines regarding the significant mirror geometry factors will be determined which may help to reduce vehicle development time and cost in the future. The results of this research will also allow us to estimate the trade-off between cost saving and performance optimum related to using a standard mirror shape for different vehicles.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2011년도 정기총회 및 추계학술대회 논문집
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• pp.663-669
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• 2011

Since railway vehicle's improvements on speed and weight has caused interior noise, the passenger's convenience fell dramatically. Therefore many on-going researches are dedicated to reduce interior noise. In this study the analytical prediction of interior noise reduction has done through filling up the empty space using form and to modify the floor structure, which contributes highly with interior noises. Using Statistical Energy Analysis(SEA), the interior noise of the vehicles without the form filling on the floor structure and the vehicles with form filling and also a modified structure has been predicted. The selected percentage of form filling was 0, 50, 100% and through this research the analysis of noise reduction by form filling has been made. When floor structure has been filled with form, approximately 2 dB of noise reduction was observed and the difference of noise reduction level with 50 and 100% form filling was predicted to be very little. Through this study, the expectation of interior noise reduction in high speed trains is considered high.