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Abstract

A small-scale three-degree-of-freedom decompression launch experiment method is used to study the flow characteristics in a ventilated cavity at different transverse velocities. The study subjects are three typical head-shaped underwater vehicles: hemispherical, ellipsoidal, and conical. The evolution mechanism of the ventilated shoulder cavity in a vehicle under transverse velocity is investigated, and the effects of transverse velocity and vehicle head shape changes on the cavity are summarized. Research results show that the hemispherical-headed vehicle’s ventilated cavity is prone to cavity pre-positioning, thereby affecting the distribution of the confronted stream surface (CSS) cavity. As the transverse velocity increases, the cavity pre-positioning point disappears, and the degree of deflection in the vehicle’s trajectory increases. The difference between the opposing stream surface (OSS) and the CSS cavities decreases as the cavities shed. The drag effect of the shedding air mass causes a change in the cavity closure angle. At high transverse velocity (vt = 0.6 m/s), the cavity difference between the OSS and CSS of the ellipsoidal vehicle is the largest, and the amount of gas shed at the cavity’s end is the smallest. The initial angle of the closure angle at the cavity end is related to the ability of the air mass near the tube (AMNT) to be drawn in by the head shape of the vehicle. Under the influence of transverse velocity, the shedding cavity deflects toward the OSS. The interaction patterns between the shoulder and tail cavities on vehicles with different head shapes primarily include three modes.

Details

1009240
Title
Experimental Study on Three-Degree-of-Freedom Ventilated Cavities for Underwater Vehicles Considering the Air Mass near the Tube
Author
Wang Jiazhao 1 ; Shi, Dongyan 2 ; Ma Guihui 3 ; Lu Jiaxing 3 ; Wang Runtian 1 

 College of Mechanical and Electrical Engineering, Harbin Engineering University, Harbin 150001, China, Innovation Center for Cross-Media Aircraft Technology, Harbin 150001, China 
 College of Mechanical and Electrical Engineering, Harbin Engineering University, Harbin 150001, China 
 Innovation Center for Cross-Media Aircraft Technology, Harbin 150001, China, College of Shipbuilding Engineering, Harbin Engineering University, Harbin 150001, China 
Volume
13
Issue
11
First page
2111
Number of pages
23
Publication year
2025
Publication date
2025
Publisher
MDPI AG
Place of publication
Basel
Country of publication
Switzerland
Publication subject
e-ISSN
20771312
Source type
Scholarly Journal
Language of publication
English
Document type
Journal Article
Publication history
 
 
Online publication date
2025-11-06
Milestone dates
2025-10-16 (Received); 2025-11-05 (Accepted)
Publication history
 
 
   First posting date
06 Nov 2025
ProQuest document ID
3275540735
Document URL
https://www.proquest.com/scholarly-journals/experimental-study-on-three-degree-freedom/docview/3275540735/se-2?accountid=208611
Copyright
© 2025 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (https://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.
Last updated
2025-11-26
Database
ProQuest One Academic