축대칭 몰수체의 유효반류 추정Prediction of the Effective Wake of an Axisymmetric Body
- Other Titles
- Prediction of the Effective Wake of an Axisymmetric Body
- Authors
- 김기섭; 문일성; 안종우; 김건도; 박영하; 이창섭
- Issue Date
- 2019
- Publisher
- 대한조선학회
- Keywords
- Axisymmetric body(축대칭 몰수체); Effective wake(유효반류); Propeller induced velocity(프로펠러 유기속도); Large Cavitation Tunnel(LCT; 대형 캐비테이션터널); VLM method(보오텍스 격자법); Vortex Tube Actuator model(VTA; 보오텍스 유관 작동판모형)
- Citation
- 대한조선학회 논문집, v.56, no.5, pp 410 - 417
- Pages
- 8
- Journal Title
- 대한조선학회 논문집
- Volume
- 56
- Number
- 5
- Start Page
- 410
- End Page
- 417
- URI
- https://www.kriso.re.kr/sciwatch/handle/2021.sw.kriso/378
- DOI
- 10.3744/SNAK.2019.56.5.410
- ISSN
- 1225-1143
- Abstract
- An axisymmetric submerged body(L=5.6m, Diam=0.53m) is installed in Large Cavitation Tunnel (LCT) of KRISO and the nominal and total velocities without and with the propeller in operation, respectively, are measured using Laser Doppler Velocimeter (LDV). The flow field is nearly axisymmetric except the wake of the supporting strut, and is considered ideal to study the hydrodynamic interaction between the propeller and the oncoming axisymmetric sheared flow. The measured velocity data are then provided to compute the propeller-induced velocity to get the effective velocity, which is defined by subtracting the propeller-induced velocity from the total velocity. We adopted, in computing the induced velocity, two different methods including the vortex lattice method and the vortex tube actuator model to evaluate the resultant effective velocity distribution.
To secure a fundamental base of experimental data necessary for the research on the effective wake, we measured the drag of the submerged body, the nominal and total velocity distributions at various axial locations for three different tunnel water speeds.
- Files in This Item
- There are no files associated with this item.
- Appears in
Collections - 선박연구본부 > Naval Ship Engineering Research Center > 1. Journal Articles
Items in ScholarWorks are protected by copyright, with all rights reserved, unless otherwise indicated.