대형 캐비테이션터널에서 몰수체 저항시험 및 위벽효과 수정 기법 연구Study of the Resistance Test and Wall Blockage Correction Method for the Submerged Body in LCT
- Other Titles
- Study of the Resistance Test and Wall Blockage Correction Method for the Submerged Body in LCT
- Authors
- 안종우; 설한신; 박영하; 김기섭
- Issue Date
- 2020
- Publisher
- 대한조선학회
- Keywords
- 대형캐비테이션터널); Submerged body(몰수체); Resistance test(저항시험); Wall blockage correction(벽면효과 수정); Large Cavitation Tunnel(LCT
- Citation
- 대한조선학회 논문집, v.57, no.3, pp 133 - 139
- Pages
- 7
- Journal Title
- 대한조선학회 논문집
- Volume
- 57
- Number
- 3
- Start Page
- 133
- End Page
- 139
- URI
- https://www.kriso.re.kr/sciwatch/handle/2021.sw.kriso/262
- DOI
- 10.3744/SNAK.2020.57.3.133
- ISSN
- 1225-1143
- Abstract
- In order to study the resistance test technique for the submerged body in Large Cavitation Tunnel (LCT), DARPA Suboff, submarine model publicly available was manufactured. DTRC released the resistance test data of DARPA Suboff conducted at ship speeds up to 18.0 knots in high-speed towing tank in 1990. As LCT is considered restricted waterways with walls, the resistance test results must be corrected with three wall blockage effects called buoyancy effect, solid blockage effect and wake blockage effect. Before correction, the resistance of LCT was 16~20 % higher than that of DTRC. After correction, the resistance and the resistance coefficients were compared with those of DTRC. The corrected resistance of LCT shows good agreement with that of DTRC. The residual resistance coefficient shows the difference according to the calculation method of buoyancy and frictional resistance coefficient. This paper suggests the best way for the calculation of residual resistance coefficient, On the basis of the present study, it is thought that the operating conditions for the propeller cavitation and noise tests can be drawn through LCT tests.
- 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.