날개 끝단 부착 프로펠러와 날개 간의 공기역학적 상호작용 효과에 대한 전산해석
The next-generation sustainable aircraft using distributed electric propulsion (DEP) system has gained significant attention to replace conventional aircraft. Although the DEP system helps improve flight safety, reduce environmental noise, and achieve redundancy in the propulsion system, the mutual...
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Published in | 한국전산유체공학회지 Vol. 29; no. 2; pp. 47 - 61 |
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Main Authors | , , , , , |
Format | Journal Article |
Language | Korean |
Published |
한국전산유체공학회
01.06.2024
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Subjects | |
Online Access | Get full text |
ISSN | 1598-6071 1598-6071 |
DOI | 10.6112/kscfe.2024.29.2.047 |
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Summary: | The next-generation sustainable aircraft using distributed electric propulsion (DEP) system has gained significant attention to replace conventional aircraft. Although the DEP system helps improve flight safety, reduce environmental noise, and achieve redundancy in the propulsion system, the mutual interaction between the multiple propeller and fixed-wing occurs more frequently. This interactional phenomenon is a dominant factor affecting the aerodynamic performance of vehicles. This study investigates the aerodynamic interactions between wing-tip mounted tractor propeller and fixed-wing using the lattice-Boltzmann method (LBM). NASA's Workshop for Integrated Propeller Prediction (WIPP) model is considered, and the LBM predictions are compared against the experimental data for validation. The propeller wake effects on the wing aerodynamics and flow field are discussed depending on the wing angles of attack. KCI Citation Count: 1 |
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ISSN: | 1598-6071 1598-6071 |
DOI: | 10.6112/kscfe.2024.29.2.047 |