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某型登陆舰的舰面流场仿真与分析
引用本文:胡国才,徐广,章晓冬.某型登陆舰的舰面流场仿真与分析[J].海军航空工程学院学报,2013,28(4):389-393.
作者姓名:胡国才  徐广  章晓冬
作者单位:[1]海军航空工程学院飞行器工程系,山东烟台264001 [2]91079部队,江苏常州213131
基金项目:国家自然科学基金(50876041);南京航空航天大学基本科研业务费专项科研项目(NS2010045)。
摘    要:舰载直升机是登陆舰实现"垂直登陆"的主要武器,研究舰面流场特性对直升机安全性能与操纵性都有重要意义。建立了某型登陆舰的三维模型,以风向角为30°,风速为15m/s的流场为例,通过数值仿真得到了飞行甲板上方的气流分布,经分析机库陡壁效应引起的下冲气流分量在机库后方形成了涡流区,在直升机的起降过程中应避免通过该涡流区,以保障直升机的安全起降、平稳飞行。

关 键 词:舰面流场  登陆舰  舰面起降  数值仿真
收稿时间:2012/4/14 0:00:00
修稿时间:2012/11/14 0:00:00

Simulation and Analysis of Flight Deck Airflow for a Certain Landing Ship
HU Guo-cai,XU Guang and ZHANG Xiao-dong.Simulation and Analysis of Flight Deck Airflow for a Certain Landing Ship[J].Journal of Naval Aeronautical Engineering Institute,2013,28(4):389-393.
Authors:HU Guo-cai  XU Guang and ZHANG Xiao-dong
Institution:1. Department of Airborne Vehicle Engineering, NAAU, Yantai Shandong 264001, China; 2. The 91079th Unit of PLA, Changzhou Jiangsu 213131, China)
Abstract:Shipboard helicopter is an important vertical landing weapon for landing ship. Research on flight deck airflow is of great significance to the control and safety of the helicopter. With three-dimensional model of a certain landing ship established, the airflow distributions in flight deck were calculated by simulation in the condition of wind angle 30°and speed 15 m/s, the analysis of which showed that the downwash from han- gar steep face made the vortex area behind the hangar. The helicopter should avoid this area when taking off and landing for the safety and steady flight.
Keywords:flight deck airflow  landing ship  take off and landing from warship  numerical simulation
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