Experimental study of air layer drag reduction of self-propelled model

ObjectivesThis paper explores the effects of air flow rate and sailing angle on the air layer retention and energy efficiency of the bottom groove of a ship, focusing on a large scale model of a bulk carrier. MethodsAn air layer drag reduction self-propelled model system and hull cavity scheme are d...

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Main Authors: Hao WU, Ziye YANG, Jianxin CAO, Yongpeng OU
Format: Article
Language:English
Published: Editorial Office of Chinese Journal of Ship Research 2024-10-01
Series:Zhongguo Jianchuan Yanjiu
Subjects:
Online Access:http://www.ship-research.com/en/article/doi/10.19693/j.issn.1673-3185.03360
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author Hao WU
Ziye YANG
Jianxin CAO
Yongpeng OU
author_facet Hao WU
Ziye YANG
Jianxin CAO
Yongpeng OU
author_sort Hao WU
collection DOAJ
description ObjectivesThis paper explores the effects of air flow rate and sailing angle on the air layer retention and energy efficiency of the bottom groove of a ship, focusing on a large scale model of a bulk carrier. MethodsAn air layer drag reduction self-propelled model system and hull cavity scheme are designed, and drag reduction experiments are conducted under open water conditions. The jet drag reduction effect on the model in a positive floating attitude of ship is examined, as well as the impact of a certain trim angle on the speed and shaft power of the model. Results The results indicate that, when the main engine speed is constant, air injection can significantly improve the speed of model; after stopping the jet, the air layer within the air cavity of the bottom groove can be maintained for a long time, with better drag reduction efficiency when the ship is in an upright state and the trimming is within 0.25 degrees. When the trimming angle is too large, the gas will overflow from both sides of the model head and the air layer will not effectively cover the bottom of the ship, decreasing the efficiency of drag reduction. ConclusionsSeveral meaningful conclusions are obtained from the above experiments, providing useful references for the engineering application of air layer drag reduction technology on full-formed ships.
format Article
id doaj-art-07a521208cd4483aba302940c6cf8335
institution Kabale University
issn 1673-3185
language English
publishDate 2024-10-01
publisher Editorial Office of Chinese Journal of Ship Research
record_format Article
series Zhongguo Jianchuan Yanjiu
spelling doaj-art-07a521208cd4483aba302940c6cf83352024-11-08T09:59:41ZengEditorial Office of Chinese Journal of Ship ResearchZhongguo Jianchuan Yanjiu1673-31852024-10-01195434810.19693/j.issn.1673-3185.03360ZG3360Experimental study of air layer drag reduction of self-propelled modelHao WU0Ziye YANG1Jianxin CAO2Yongpeng OU3Key Laboratory of High Performance Ship Technology, Ministry of Education, Wuhan University of Technology, Wuhan 430063, ChinaKey Laboratory of High Performance Ship Technology, Ministry of Education, Wuhan University of Technology, Wuhan 430063, ChinaKey Laboratory of High Performance Ship Technology, Ministry of Education, Wuhan University of Technology, Wuhan 430063, ChinaCollege of Naval Architecture and Ocean Engineering, Naval University of Engineering, Wuhan 430033, ChinaObjectivesThis paper explores the effects of air flow rate and sailing angle on the air layer retention and energy efficiency of the bottom groove of a ship, focusing on a large scale model of a bulk carrier. MethodsAn air layer drag reduction self-propelled model system and hull cavity scheme are designed, and drag reduction experiments are conducted under open water conditions. The jet drag reduction effect on the model in a positive floating attitude of ship is examined, as well as the impact of a certain trim angle on the speed and shaft power of the model. Results The results indicate that, when the main engine speed is constant, air injection can significantly improve the speed of model; after stopping the jet, the air layer within the air cavity of the bottom groove can be maintained for a long time, with better drag reduction efficiency when the ship is in an upright state and the trimming is within 0.25 degrees. When the trimming angle is too large, the gas will overflow from both sides of the model head and the air layer will not effectively cover the bottom of the ship, decreasing the efficiency of drag reduction. ConclusionsSeveral meaningful conclusions are obtained from the above experiments, providing useful references for the engineering application of air layer drag reduction technology on full-formed ships.http://www.ship-research.com/en/article/doi/10.19693/j.issn.1673-3185.03360self-propelled modelair injection deviceair layer maintenancedrag reductionenergy conservation
spellingShingle Hao WU
Ziye YANG
Jianxin CAO
Yongpeng OU
Experimental study of air layer drag reduction of self-propelled model
Zhongguo Jianchuan Yanjiu
self-propelled model
air injection device
air layer maintenance
drag reduction
energy conservation
title Experimental study of air layer drag reduction of self-propelled model
title_full Experimental study of air layer drag reduction of self-propelled model
title_fullStr Experimental study of air layer drag reduction of self-propelled model
title_full_unstemmed Experimental study of air layer drag reduction of self-propelled model
title_short Experimental study of air layer drag reduction of self-propelled model
title_sort experimental study of air layer drag reduction of self propelled model
topic self-propelled model
air injection device
air layer maintenance
drag reduction
energy conservation
url http://www.ship-research.com/en/article/doi/10.19693/j.issn.1673-3185.03360
work_keys_str_mv AT haowu experimentalstudyofairlayerdragreductionofselfpropelledmodel
AT ziyeyang experimentalstudyofairlayerdragreductionofselfpropelledmodel
AT jianxincao experimentalstudyofairlayerdragreductionofselfpropelledmodel
AT yongpengou experimentalstudyofairlayerdragreductionofselfpropelledmodel