Detailed Information
Cited 0 time in 
Cited 0 time in 
Cited 0 time in
Metadata Downloads
NACA 4412 날개의 지면효과에 대한 2차원 공력 해석
Full metadata record
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | 김윤식 | - |
| dc.contributor.author | 이재은 | - |
| dc.contributor.author | 신명수 | - |
| dc.contributor.author | 강국진 | - |
| dc.contributor.author | 권장혁 | - |
| dc.date.accessioned | 2021-12-08T22:41:08Z | - |
| dc.date.available | 2021-12-08T22:41:08Z | - |
| dc.date.issued | 20061013 | - |
| dc.identifier.uri | https://www.kriso.re.kr/sciwatch/handle/2021.sw.kriso/6660 | - |
| dc.description.abstract | Two dimensional turbulent flow simulations on the low Mach number － high Reynolds number flow about the NACA 4412 airfoil are carried out as the airfoil approaches a ground. It has been turned out that angle of attack between 2 and 8 is recommended for the airfoil to utilize the benefit of ground effect. For the large angle of attack, the increment of lift due to the ground effect is eliminated and negative aerodynamic effect such as destabilizing aspect in static longitudinal stability are occurred as the airfoil approaches a ground. | - |
| dc.language | 한국어 | - |
| dc.language.iso | KOR | - |
| dc.title | NACA 4412 날개의 지면효과에 대한 2차원 공력 해석 | - |
| dc.title.alternative | 2-Dimensional Aerodynamic Simulation on the Ground Effect of the NACA 4412 Airfoil | - |
| dc.type | Conference | - |
| dc.citation.title | 한국전산유체공학회 추계학술대회 | - |
| dc.citation.volume | 1 | - |
| dc.citation.number | 1 | - |
| dc.citation.startPage | 199 | - |
| dc.citation.endPage | 205 | - |
| dc.citation.conferenceName | 한국전산유체공학회 추계학술대회 | - |
- Files in This Item
- There are no files associated with this item.
- Appears in
Collections - ETC > 2. Conference Papers
Items in ScholarWorks are protected by copyright, with all rights reserved, unless otherwise indicated.