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논문 기본정보
반응표면법을 이용한 축류 압축기의 동익형상 최적설계
논문 개요
| 기관명 | NDSL |
|---|---|
| 저널명 | 한국유체기계학회 논문집 = The KSFM journal of fluid machinery |
| ISSN | 2287-9706, |
| ISBN |
논문저자 및 소속기관 정보
| 저자(한글) | 송유준,이정민,김윤제 |
|---|---|
| 저자(영문) | |
| 소속기관 | |
| 소속기관(영문) | |
| 출판인 | |
| 간행물 번호 | |
| 발행연도 | 2016-01-01 |
| 초록 | Design optimization of a transonic compressor rotor(NASA rotor 37) was carried out using response surface method(RSM) which is one of the optimization methods. A numerical simulation was conducted using ANSYS CFX by solving three-dimensional Reynolds-averaged Navier Stokes(RANS) equations. Response surfaces that were based on the results of the design of experiment(DOE) techniques were used to find an optimal shape of blade which has the maximum aerodynamic performance. Two objective functions, viz., the adiabatic efficiency and the loss coefficient were selected with three design configurations to optimize the blade shape. As a result, the efficiency of the optimized blade is found to be increased. |
| 원문URL | http://click.ndsl.kr/servlet/OpenAPIDetailView?keyValue=03553784&target=NART&cn=JAKO201613360957665 |
| 첨부파일 |
추가정보
| 과학기술표준분류 | |
|---|---|
| ICT 기술분류 | |
| DDC 분류 | |
| 주제어 (키워드) | 축류 압축기,반응 표면법,최적설계,실험계획법,Axial Compressor,Response Surface Method,Optimal Design,Design of Experiment |