• 제목/요약/키워드: Local Regression Rate

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하이브리드 로켓에서의 고체연료의 국부 후퇴율에 관한 연구 (A Study on the Local Regression Rate of Solid Fuel in Hybrid Rocket)

  • 김수종;이정표;김기훈;조정태;김학철;우경진;문희장;성홍계;김진곤
    • 항공우주시스템공학회지
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    • 제2권4호
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    • pp.1-6
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    • 2008
  • In generally, the regression rate was expressed with average value and oxidizer mass flux in hybrid propulsion system. This can not represent the local value of regression rate along with oxidizer flow direction. In this study, experimental studies were performed with Separation method and Cutting method for measure local regression rate. In axial injection, the local regression rate decreases rapidly with axial location near entrance and increases with axial direction from the leading edge and the empirical formula for local regression rate with function of oxidizer mass flux and location was derived. Swirl injection regression rate has higher value at the leading edge of the fuel and comparatively uniform regression rate at the downstream. Overall regression rate of swirl injection is higher increased about 54 % than regression rate of axial injection.

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지리적가중회귀분석을 이용한 관외입원진료비 비율의 지역 간 차이 분석 (Analysis on the Regional Variation of the Rate of Inpatient Medical Costs in Local-Out: Geographically Weighted Regression Approach)

  • 조은경;이광수
    • 보건의료산업학회지
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    • 제8권2호
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    • pp.11-22
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    • 2014
  • This study purposed to analyze the regional variation of the local-out rates of inpatient services. Multiple data sources collected from National Health Insurance Corporation and statistics Korea were merged to produce the analysis data set. The unit of analysis in this study was city, Gun, Gu, and all of them were included in analysis. The dependent variable measured the local-out rate of inpatient cost in study regions. Local environments were measured by variables in three dimensions: provider factors, socio-demographic factors, and health status. Along with the traditional ordinary least square (OLS) based regression model, geographically weighted regression (GWR) model were applied to test their effects. SPSS v21 and ArcMap v10.2 were applied for the statistical analysis. Results from OLS regression showed that most variables had significant relationships with the local-out rate of inpatient services. However, some variables had shown diverse directions in regression coefficients depending on regions in GWR. This implied that the study variables might not have consistent effects and they may varied depending the locations.

스월 인젝션 하이브리드 로켓의 고체연료 국부 후퇴율에 관한 연구 (A Study on the Local Regression Rate of Solid Fuel in Swirl Injection Hybrid Rocket)

  • 김수종;이정표;김기훈;조정태;문희장;성홍계;김진곤
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년도 제30회 춘계학술대회논문집
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    • pp.77-81
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    • 2008
  • 스월 인젝션 하이브리드 로켓의 고체연료에서 축 방향 국부 후퇴율 거동을 고찰하였다. 일반적으로 축 인젝션 후퇴율은 연료 그레인 축 위치가 입구에서 멀어질수록 감소하다가, 다시 증가하는 경향을 보인다. 이에 반해 스월 인젝션 후퇴율은 연료 입구부에서 높고, 하류에서는 비교적 균일한 후퇴율을 보임을 확인하였다. 전체 후퇴율은 스월 인젝션의 경우가 축 인젝션의 경우에 비해 54% 증가하였다. 본 연구를 통해 소형 사운딩 로켓에서 스월 인젝터를 사용하는 것이 유용할 수 있음을 확인하였다.

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하이브리드 로켓에서의 고체연료의 국부 후퇴율에 관한 연구 (A Study on the Local Regression Rate of Solid Fuel in Hybrid Rocket)

  • 이정표;김기훈;조정태;김수종;문희장;성홍계;김진곤
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년도 제30회 춘계학술대회논문집
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    • pp.89-92
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    • 2008
  • 일반적으로 하이브리드 추진에서 산화제 질량유속만의 함수로 표현되는 후퇴율 식은 고체연료 길이에 따른 후퇴율 변화를 나타내지 못한다. 따라서 본 연구에서는 분할 연료 그레인을 적용해 쉽게 할 수 있는 연소 실험을 수행했고, 고체연료 길이에 따른 후퇴율의 변화를 고찰하였다. 연료 그레인 상단부에서 하단부로 갈수록 후퇴율은 감소하다가, 다시 증가하는 경향을 나타남을 확인 하였고, 산화제 질량유속과 그레인 길이의 함수로 표현할 수 있는 후퇴율 식을 도출하였다.

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ON MARGINAL INTEGRATION METHOD IN NONPARAMETRIC REGRESSION

  • Lee, Young-Kyung
    • Journal of the Korean Statistical Society
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    • 제33권4호
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    • pp.435-447
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    • 2004
  • In additive nonparametric regression, Linton and Nielsen (1995) showed that the marginal integration when applied to the local linear smoother produces a rate-optimal estimator of each univariate component function for the case where the dimension of the predictor is two. In this paper we give new formulas for the bias and variance of the marginal integration regression estimators which are valid for boundary areas as well as fixed interior points, and show the local linear marginal integration estimator is in fact rate-optimal when the dimension of the predictor is less than or equal to four. We extend the results to the case of the local polynomial smoother, too.

Factors Related to Regional Variation in the High-risk Drinking Rate in Korea: Using Quantile Regression

  • Kim, Eun-Su;Nam, Hae-Sung
    • Journal of Preventive Medicine and Public Health
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    • 제54권2호
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    • pp.145-152
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    • 2021
  • Objectives: This study aimed to identify regional differences in the high-risk drinking rate among yearly alcohol users in Korea and to identify relevant regional factors for each quintile using quantile regression. Methods: Data from 227 counties surveyed by the 2017 Korean Community Health Survey (KCHS) were analyzed. The analysis dataset included secondary data extracted from the Korean Statistical Information Service and data from the KCHS. To identify regional factors related to the high-risk drinking rate among yearly alcohol users, quantile regression was conducted by dividing the data into 10%, 30%, 50%, 70%, and 90% quantiles, and multiple linear regression was also performed. Results: The current smoking rate, perceived stress rate, crude divorce rate, and financial independence rate, as well as one's social network, were related to the high-risk drinking rate among yearly alcohol users. The quantile regression revealed that the perceived stress rate was related to all quantiles except for the 90% quantile, and the financial independence rate was related to the 50% to 90% quantiles. The crude divorce rate was related to the high-risk drinking rate among yearly alcohol users in all quantiles. Conclusions: The findings of this study suggest that local health programs for high-risk drinking are needed in areas with high local stress and high crude divorce rates.

국부연소 후퇴율을 고려한 하이브리드로켓의 성능예측 기법연구 (Performance Prediction Method of Hybrid Rocket Motors with Local Variance of Combustion)

  • 조민경;허준영;박형주;김진곤;문희장;성홍계
    • 한국추진공학회지
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    • 제16권1호
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    • pp.9-15
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    • 2012
  • 하이브리드 연소실의 국부 압력과 속도변화를 고려하는 비정상 내탄도 해석모델을 제안하고 이를 바탕으로 연소실 내 국부영역에서 내탄도 특성인자의 변화를 도출하였다. 해석 모델 검증을 위하여 연소실 전후단의 압력을 측정한 실험결과와 해석결과를 비교하여 실험과 해석결과가 유사함을 확인하고 연소 효율을 평가 하였다. 하류방향으로 산화제 유량이 변화하므로 이에 따른 연소실 국부영역의 압력, 온도, 연료의 후퇴율 및 연소가스의 유속 변화를 정량적으로 고찰하였다.

Study on semi-supervised local constant regression estimation

  • Seok, Kyung-Ha
    • Journal of the Korean Data and Information Science Society
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    • 제23권3호
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    • pp.579-585
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    • 2012
  • Many different semi-supervised learning algorithms have been proposed for use wit unlabeled data. However, most of them focus on classification problems. In this paper we propose a semi-supervised regression algorithm called the semi-supervised local constant estimator (SSLCE), based on the local constant estimator (LCE), and reveal the asymptotic properties of SSLCE. We also show that the SSLCE has a faster convergence rate than that of the LCE when a well chosen weighting factor is employed. Our experiment with synthetic data shows that the SSLCE can improve performance with unlabeled data, and we recommend its use with the proper size of unlabeled data.

RATO(Rocket-Assisted Take Off) 시스템 적용을 위한 하이브리드 로켓 비단공형 연료 그레인 기초 연소특성 연구 (A Study on Combustion Characteristics of Non-Circular Grain in Hybrid Rocket for RATO (Rocket-Assisted Take Off) System)

  • 김수진;고수한;김설희;김경모;이성근;한예찬;문희장
    • 한국항공운항학회지
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    • 제30권4호
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    • pp.184-190
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    • 2022
  • In an attempt to apply hybrid rocket to the RATO (Rocket-Assisted Take Off) system, combustion characteristics of the non-circular grain were figured out in this study. Having larger combustion area, it was reconfirmed that the non-circular grain has advantages over regression rate, characteristic velocity and chamber pressure in which all gave higher values. Experiments were performed to understand the effect of the non-circular grain geometry over time where local regression rates depending on grain location were analyzed. It was found that the regression rate of five distinct locations were different. Partial conclusion driven was that these differences are due to the heat transfer caused by dissimilar distances from the flame layer. Besides, as combustion duration increased, the fuel port became circular, and the regression rate converged to a single value over the whole grain.

하이브리드 로켓 연료의 국부 후퇴율 측정기법에 관한 연구 (A Study on the Measurement Technique for Local Regression rate of Solid fuel in Hybrid rocket)

  • 조정태;김기훈;우경진;김수종;이정표;김학철;성홍계;문희장;김진곤
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2009년도 춘계학술대회 논문집
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    • pp.243-246
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    • 2009
  • 하이브리드 로켓의 고체 연료에서 축방향 국부 후퇴율은 하이브리드 추진 연소기의 설계 변수 및 성능 변수로 활용 된다. 국부 후퇴율 측정하기 위한 방법으로는 여러 가지 있지만, 침수법은 간단한 방법으로 연료의 형상 및 물리적 특성에 관계 없이 정확하게 축방향 국부 후퇴율을 측정할 수 있다. 본 연구에서는 기존의 국부 후퇴율 측정장비의 문제점을 개선하였고, 실험을 통해 높은 정확성을 가짐을 확인 하였다.

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